B COUNCIL REGULATION (EU) No 267/2012 of 23 March 2012 Concerning Restrictive Measures Against Iran and Repealing Regulation (EU) No 961/2010 (OJ L 88, 24.3.2012, P

02012R0267 — EN — 18.01.2017 — 022.003 — 1

This text is meant purely as a documentation tool and has no legal effect. The Union's institutions do not assume any liability for its contents. The authentic versions of the relevant acts, including their preambles, are those published in the Official Journal of the European Union and available in EUR-Lex. Those official texts are directly accessible through the links embedded in this document

►B COUNCIL REGULATION (EU) No 267/2012 of 23 March 2012 concerning restrictive measures against Iran and repealing Regulation (EU) No 961/2010 (OJ L 88, 24.3.2012, p. 1)

Amended by:

Official Journal

No page date ►M1 Council Implementing Regulation (EU) No 350/2012 of 23 April 2012 L 110 17 24.4.2012

►M2 Council Regulation (EU) No 708/2012 of 2 August 2012 L 208 1 3.8.2012

►M3 Council Implementing Regulation (EU) No 709/2012 of 2 August 2012 L 208 2 3.8.2012

►M4 Council Implementing Regulation (EU) No 945/2012 of 15 L 282 16 16.10.2012 October 2012

►M5 Council Implementing Regulation (EU) No 1016/2012 of 6 L 307 5 7.11.2012 November 2012

►M6 Council Regulation (EU) No 1067/2012 of 14 November 2012 L 318 1 15.11.2012

►M7 Council Regulation (EU) No 1263/2012 of 21 December 2012 L 356 34 22.12.2012

►M8 Council Implementing Regulation (EU) No 1264/2012 of 21 L 356 55 22.12.2012 December 2012

►M9 Council Implementing Regulation (EU) No 522/2013 of 6 June 2013 L 156 3 8.6.2013

►M10 Council Regulation (EU) No 517/2013 of 13 May 2013 L 158 1 10.6.2013

►M11 Council Regulation (EU) No 971/2013 of 10 October 2013 L 272 1 12.10.2013

►M12 Council Implementing Regulation (EU) No 1154/2013 of 15 L 306 3 16.11.2013 November 2013

►M13 Council Implementing Regulation (EU) No 1203/2013 of 26 L 316 1 27.11.2013 November 2013

►M14 Council Implementing Regulation (EU) No 1361/2013 of 17 L 343 7 19.12.2013 December 2013

►M15 Council Regulation (EU) No 42/2014 of 20 January 2014 L 15 18 20.1.2014

►M16 Council Implementing Regulation (EU) No 397/2014 of 16 April 2014 L 119 1 23.4.2014

►M17 Council Implementing Regulation (EU) No 1202/2014 of 7 L 325 3 8.11.2014 November 2014 02012R0267 — EN — 18.01.2017 — 022.003 — 2

►M18 Council Regulation (EU) 2015/229 of 12 February 2015 L 39 1 14.2.2015 ►M19 Council Implementing Regulation (EU) 2015/230 of 12 L 39 3 14.2.2015 February 2015 ►M20 Council Implementing Regulation (EU) 2015/549 of 7 April 2015 L 92 12 8.4.2015

►M21 Council Implementing Regulation (EU) 2015/1001 of 25 June 2015 L 161 1 26.6.2015

►M22 Council Regulation (EU) 2015/1327 of 31 July 2015 L 206 18 1.8.2015

►M23 Council Regulation (EU) 2015/1328 of 31 July 2015 L 206 20 1.8.2015

►M24 Council Regulation (EU) 2015/1861 of 18 October 2015 L 274 1 18.10.2015

►M25 Council Implementing Regulation (EU) 2015/1862 of 18 October 2015 L 274 161 18.10.2015

►M26 Council Implementing Regulation (EU) 2015/2204 of 30 November L 314 10 1.12.2015 2015

►M27 Council Regulation (EU) 2016/31 of 14 January 2016 L 10 1 15.1.2016

►M28 Council Implementing Regulation (EU) 2016/74 of 22 January 2016 L 16 6 23.1.2016

►M29 Council Implementing Regulation (EU) 2016/603 of 18 April 2016 L 104 8 20.4.2016

►M30 Commission Implementing Regulation (EU) 2016/1375 of 29 July 2016 L 221 1 16.8.2016

►M31 Council Implementing Regulation (EU) 2017/77 of 16 January 2017 L 12 24 17.1.2017

Corrected by:

►C1 Corrigendum, OJ L 332, 4.12.2012, p. 31 (267/2012) ►C2 Corrigendum, OJ L 41, 12.2.2013, p. 14 (709/2012) ►C3 Corrigendum, OJ L 268, 10.10.2013, p. 18 (1264/2012) ►C4 Corrigendum, OJ L 93, 28.3.2014, p. 85 (267/2012)

The presentation of this consolidated text takes into account judgments of the EU Courts concerning entries in the list of designated persons and entities. 02012R0267 — EN — 18.01.2017 — 022.003 — 3

▼B COUNCIL REGULATION (EU) No 267/2012 of 23 March 2012 concerning restrictive measures against Iran and repealing Regulation (EU) No 961/2010

CHAPTER I DEFINITIONS

Article 1

For the purposes of this Regulation the following definitions shall apply:

(a) 'branch' of a financial or credit institution means a place of business which forms a legally dependent part of a financial or credit insti tution and which carries out directly all or some of the transactions inherent in the business of financial or credit institutions;

(b) 'brokering services' means:

(i) the negotiation or arrangement of transactions for the purchase, sale or supply of goods and technology or of financial and technical services, including from a third country to any other third country, or

(ii) the selling or buying of goods and technology or of financial and technical services, including where they are located in third countries for their transfer to another third country;

(c) 'claim' means any claim, whether asserted by legal proceedings or not, made before or after the date of entry into force of this Regu lation, under or in connection with a contract or transaction, and includes in particular:

(i) a claim for performance of any obligation arising under or in connection with a contract or transaction;

(ii) a claim for extension or payment of a bond, financial guarantee or indemnity of whatever form;

(iii) a claim for compensation in respect of a contract or transaction;

(iv) a counterclaim;

(v) a claim for the recognition or enforcement, including by the procedure of exequatur, of a judgment, an arbitration award or an equivalent decision, wherever made or given;

(d) 'contract or transaction' means any transaction of whatever form and whatever the applicable law, whether comprising one or more contracts or similar obligations made between the same or different parties; for this purpose 'contract' includes a bond, guarantee or indemnity, particularly a financial guarantee or financial indemnity, and credit, whether legally independent or not, as well as any related provision arising under, or in connection with, the transaction; 02012R0267 — EN — 18.01.2017 — 022.003 — 4

▼B (e) 'competent authorities' refers to the competent authorities of the Member States as identified on the websites listed in Annex X;

(f) 'credit institution' means a credit institution as defined in Article 4(1) of Directive 2006/48/EC of the European Parliament and of the Council of 14 June 2006 relating to the taking up and pursuit of the business of credit institutions (1 ), including its branches inside or outside the Union;

(g) 'customs territory of the Union' means the territory as defined in Article 3 of Council Regulation (EEC) No 2913/92 of 12 October 1992 establishing the Community Customs Code (2 ) and in Commission Regulation (EEC) No 2454/93 of 2 July 1993 laying down provisions for the implementation of Regulation (EEC) No 2913/92 (3 );

(h) 'economic resources' means assets of every kind, whether tangible or intangible, movable or immovable, which are not funds, but which may be used to obtain funds, goods or services;

(i) 'financial institution' means

(i) an undertaking, other than a credit institution, which carries out one or more of the operations included in points 2 to 12 and points 14 and 15 of Annex I to Directive 2006/48/EC, including the activities of currency exchange offices (bureaux de change);

(ii) an insurance company duly authorised in accordance with Directive 2009/138/EC of the European Parliament and of the Council of 25 November 2009 on the taking-up and pursuit of the business of Insurance and Reinsurance (Solvency II) (4 ), in so far as it carries out activities covered by that Directive;

(iii) an investment firm as defined in point 1 of Article 4(1) of Directive 2004/39/EC of the European Parliament and of the Council of 21 April 2004 on markets in financial instruments (5 );

(iv) a collective investment undertaking marketing its units or shares; or

(v) an insurance intermediary as defined in Article 2(5) of Directive 2002/92/EC of the European Parliament and of the Council of 9 December 2002 on insurance mediation (6 ), with the exception of intermediaries referred to in Article 2(7) of that Directive, when they act in respect of life insurance and other investment related services;

including its branches inside or outside the Union;

(1 ) OJ L 177, 30.6.2006, p. 1. (2 ) OJ L 302, 19.10.1992, p. 1. (3 ) OJ L 253, 11.10.1993, p. 1. (4 ) OJ L 335, 17.12.2009, p. 1. (5 ) OJ L 145, 30.4.2004, p. 1. (6 ) OJ L 9, 15.1.2003, p. 3. 02012R0267 — EN — 18.01.2017 — 022.003 — 5

▼B (j) 'freezing of economic resources' means preventing the use of economic resources to obtain funds, goods or services in any way, including, but not limited to, by selling, hiring or mortgaging them;

(k) 'freezing of funds' means preventing any move, transfer, alteration, use of, access to, or dealing with funds in any way that would result in any change in their volume, amount, location, ownership, possession, character, destination or other change that would enable the funds to be used, including portfolio management;

(l) 'funds' means financial assets and benefits of every kind, including, but not limited to:

(i) cash, cheques, claims on money, drafts, money orders and other payment instruments;

(ii) deposits with financial institutions or other entities, balances on accounts, debts and debt obligations;

(iii) publicly-and privately-traded securities and debt instruments, including stocks and shares, certificates representing secur ities, bonds, notes, warrants, debentures and derivatives contracts;

(iv) interest, dividends or other income on or value accruing from or generated by assets;

(v) credit, right of set-off, guarantees, performance bonds or other financial commitments;

(vi) letters of credit, bills of lading, bills of sale; and

(vii) documents showing evidence of an interest in funds or financial resources;

(m) 'goods' includes items, materials and equipment;

(n) 'insurance' means an undertaking or commitment whereby one or more natural or legal persons is or are obliged, in return for a payment, to provide one or more other persons, in the event of materialisation of a risk, with an indemnity or a benefit as determined by the undertaking or commitment;

(o) 'Iranian person, entity or body' means:

(i) the State of Iran or any public authority thereof;

(ii) any natural person in, or resident in, Iran; 02012R0267 — EN — 18.01.2017 — 022.003 — 6

▼B (iii) any legal person, entity or body having its registered office in Iran;

(iv) any legal person, entity or body, inside or outside Iran, owned or controlled directly or indirectly by one or more of the above mentioned persons or bodies;

(p) 'reinsurance' means the activity consisting in accepting risks ceded by an insurance undertaking or by another reinsurance undertaking or, in the case of the association of underwriters known as Lloyd's, the activity consisting in accepting risks, ceded by any member of Lloyd's, by an insurance or reinsurance undertaking other than the association of underwriters known as Lloyd's;

(q) 'Sanctions Committee' means the Committee of the United Nations Security Council which was established pursuant to paragraph 18 of United Nations Security Council Resolution ("UNSCR") 1737 (2006);

(r) 'technical assistance' means any technical support related to repairs, development, manufacture, assembly, testing, maintenance, or any other technical service, and may take forms such as instruction, advice, training, transmission of working knowledge or skills or consulting services; including verbal forms of assistance;

(s) 'territory of the Union' means the territories of the Member States to which the Treaty is applicable, under the conditions laid down in the Treaty, including their airspace;

▼M24 ______

(u) 'Joint Commission' means a joint commission consisting of repre sentatives of Iran and of China, France, Germany, the Russian Federation, the United Kingdom and the United States with the High Representative of the Union for Foreign Affairs and Security Policy (‘High Representative’), that will be established to monitor the implementation of the Joint Comprehensive Plan of Action of 14 July 2015 (‘JCPOA’) and will carry out the functions provided for in the JCPOA, in accordance with point ix of the JCPOA's ‘Preamble and General Provisions’ and Annex IV to the JCPOA.

▼B

CHAPTER II EXPORT AND IMPORT RESTRICTIONS ▼M24 ______

Article 2a

1. A prior authorisation shall be required:

(a) for the sale, supply, transfer or export, directly or indirectly, of the goods and technology listed in Annex I, whether or not originating in the Union, to any Iranian person, entity or body or for use in Iran; 02012R0267 — EN — 18.01.2017 — 022.003 — 7

▼M24 (b) for the provision of technical assistance or brokering services related to goods and technology listed in Annex I or related to the provision, manufacture, maintenance and use of goods and tech nology included in Annex I, directly or indirectly, to any Iranian person, entity or body, or for use in Iran;

(c) for the provision of financing or financial assistance related to goods and technology listed Annex I, including in particular grants, loans and export credit insurance for any sale, supply, transfer or export of such items, or for any provision of related technical assistance or brokering services, directly or indirectly, to any Iranian person, entity or body, or for use in Iran;

(d) before entering into any arrangement with an Iranian person, entity or body, or any person or entity acting on their behalf or at their direction, including the acceptance of loans or credit made by such person, entity or body, that would enable such person, entity or body to participate in or increase its participation, be that indepen dently or as part of a joint venture or other partnership, in commercial activities involving the following:

(i) uranium mining,

(ii) production or use of nuclear materials as listed in Part 1 of the Nuclear Suppliers Group list.

This shall include the making of loans or credit to such a person, entity or body;

(e) for the purchase, import or transport from Iran of goods and tech nology listed in Annex I, whether or not originating in Iran.

2. Annex I shall list the items, including goods, technology and software, contained in the Nuclear Suppliers Group list.

3. The Member State concerned shall submit the proposed authori sation under points (a) to (d) of paragraph 1 to the UN Security Council for approval on a case-by-case basis and shall not grant the authori sation until that approval has been received.

4. The Member State concerned shall also submit the proposed auth orisations of activities referred to in points (a) to (d) of paragraph 1 to the UN Security Council for approval on a case-by-case basis if the activities are related to any further goods and technology that, based on the determination by that Member State, could contribute to repro cessing- or enrichment-related or heavy water-related activities incon sistent with the JCPOA. The Member State shall not grant the auth orisation until that approval has been received.

5. The competent authority concerned shall not grant the authori sation under point (e) of paragraph 1 until it has been approved by the Joint Commission.

6. The Member State concerned shall notify the other Member States, the Commission and the High Representative of authorisations granted under paragraphs (1) and (5), or any refusal by the UN Security Council to approve an authorisation in accordance with paragraphs (3) or (4). 02012R0267 — EN — 18.01.2017 — 022.003 — 8

▼M24 Article 2b

1. Article 2a(3) and (4) do not apply in relation to proposed auth orisations for the supply, sale or transfer to Iran of equipment referred to in paragraph 2(c), subparagraph 1 of Annex B to UNSCR 2231 (2015) for light water reactors.

2. The Member State concerned shall inform the other Member States, the Commission and the High Representative, within four weeks, of authorisations granted under this Article.

Article 2c

1. The competent authorities granting an authorisation in accordance with Article 2a(1)(a) and Article 2b shall ensure the following:

(a) the requirements, as appropriate, of the Guidelines as set out in the Nuclear Suppliers Group list have been met;

(b) the rights to verify the end-use and end-use location of any supplied item have been obtained from Iran and can be exercised effectively;

(d) in the case of supplied goods and technology referred to in Annex I, the notification of the IAEA within ten days of the supply, sale or transfer.

2. For all exports for which an authorisation is required under Article 2a(1)(a), such authorisation shall be granted by the competent authorities of the Member State where the exporter is established. The authorisation shall be valid throughout the Union.

3. Exporters shall supply the competent authorities with all relevant information, as set out in Article 14(1) of Regulation (EC) No 428/2009 and as specified by each competent authority, required for their appli cation for an export authorisation.

Article 2d

1. Article 2a(3) and (4) do not apply in relation to proposed auth orisations for the supply, sale, or transfer of items, materials, equipment, goods and technology, and the provision of any related technical assistance, training, financial assistance, investment, brokering or other services where the competent authorities consider them to be directly related to the following:

(a) the necessary modification of two cascades at the Fordow facility for stable isotope production;

(b) the export of Iran's enriched uranium in excess of 300 kilograms in return for natural uranium; or

(c) the modernisation of the Arak reactor based on the agreed conceptual design and, subsequently, on the agreed final design of such reactor.

2. The competent authority granting an authorisation in accordance with paragraph 1 shall ensure the following: 02012R0267 — EN — 18.01.2017 — 022.003 — 9

▼M24 (a) all activities are undertaken strictly in accordance with the JCPOA;

(b) the requirements, as appropriate, of the Guidelines as set out in the Nuclear Suppliers Group list have been met;

(c) rights to verify the end-use and end-use location of any supplied item have been obtained from Iran and can be exercised effectively.

3. The Member State concerned shall notify:

(a) the UN Security Council and the Joint Commission ten days in advance of such activities;

(b) the IAEA within ten days of the supply, sale or transfer, in case of supplied items, materials, equipment, goods and technology included in the Nuclear Suppliers Group list.

4. The Member State concerned shall inform the other Member States, the Commission and the High Representative, within four weeks, of authorisations granted under this Article.

Article 3a

1. A prior authorisation shall be required, on a case-by-case basis:

(a) for the sale, supply, transfer or export, directly or indirectly, of the goods and technology listed in Annex II, whether or not originating in the Union, to any Iranian person, entity or body or for use in Iran;

(b) for the provision of technical assistance or brokering services related to goods and technology listed in Annex II or related to the provision, manufacture, maintenance and use of goods included in Annex II, directly or indirectly, to any Iranian person, entity or body, or for use in Iran;

(c) for the provision of financing or financial assistance related to goods and technology listed Annex II, including in particular grants, loans and export credit insurance for any sale, supply, transfer or export of such items, or for any provision of related technical assistance or brokering services, directly or indirectly, to any Iranian person, entity or body, or for use in Iran;

(e) for the purchase, import or transport from Iran of goods and tech nology listed in Annex II, whether or not originating in Iran. 02012R0267 — EN — 18.01.2017 — 022.003 — 10

▼M24 2. Annex II shall list the goods and technology, other than those included in Annexes I and III, that could contribute to reprocessing- or enrichment-related or heavy water-related or other activities incon sistent with the JCPOA.

3. Exporters shall supply the competent authorities with all relevant information required for their application for an authorisation.

4. The competent authorities shall not grant any authorisation for the transactions referred to in paragraph 1(a) to (e), if they have reasonable grounds to determine that the actions concerned would contribute to reprocessing- or enrichment-related, heavy water-related or other nuclear related activities inconsistent with the JCPOA.

5. The competent authorities shall exchange information on requests for authorisation received under this Article. The system referred to in Article 19(4) of Regulation (EC) No 428/2009 shall be used for this purpose.

6. The competent authority granting an authorisation in accordance with paragraph 1(a) shall ensure that rights to verify the end-use and end-use location of any supplied item have been obtained from Iran and can be exercised effectively.

7. The Member State concerned shall notify the other Member States, the Commission and the High Representative of its intention to grant an authorisation under this Article at least ten days prior to the authori sation.

Article 3b

1. For all exports for which an authorisation is required under Article 3a, such authorisation shall be granted by the competent auth orities of the Member State where the exporter is established and shall be in accordance with the detailed rules laid down in Article 11 of Regulation (EC) No 428/2009. The authorisation shall be valid throughout the Union.

2. Under the conditions set out in Article 3a(4) and (5), the competent authorities may annul, suspend, modify or revoke an export authorisation which they have granted.

3. Where a competent authority refuses to grant an authorisation, or annuls, suspends, substantively modifies or revokes an authorisation in accordance with Article 3a(4), the Member State concerned shall notify the other Member States, the Commission and the High Representative thereof and share the relevant information with them, while complying with the provisions concerning the confidentiality of such information of Council Regulation (EC) No 515/97 (1 ).

4. Before a competent authority of a Member State grants an authori sation in accordance with Article 3a for a transaction which is essentially identical to a transaction which is the subject of a still valid denial issued by another Member State or by other Member States under Article 3a(4), it shall first consult the Member State or Member States which issued the

(1 ) Council Regulation (EC) No 515/97 of 13 March 1997 on mutual assistance between the administrative authorities of the Member States and cooperation between the latter and the Commission to ensure the correct application of the law on customs and agricultural matters (OJ L 82, 22.3.1997, p. 1). 02012R0267 — EN — 18.01.2017 — 022.003 — 11

▼M24 denial. If, following such consultations, the Member State concerned decides to grant an authorisation, it shall inform the other Member States, the Commission and the High Representative thereof, providing all relevant information to explain the decision.

Article 3c

1. Article 3a does not apply in relation to proposed authorisations for the supply, sale or transfer to Iran of goods and technology listed in Annex II for light water reactors.

2. The competent authority granting an authorisation in accordance with paragraph 1 shall ensure that rights to verify the end-use and end- use location of any supplied item have been obtained from Iran and can be exercised effectively.

3. The Member State concerned shall inform the other Member States, the Commission and the High Representative, within four weeks, of authorisations granted under this Article.

Article 3d

1. Article 3a does not apply in relation to proposed authorisations for the supply, sale, or transfer of items, materials, equipment, goods and technology, and the provision of any related technical assistance, training, financial assistance, investment, brokering or other services where the competent authorities consider them to be directly related to the following:

(a) the necessary modification of two cascades at the Fordow facility for stable isotope production;

(b) the export of Iran's enriched uranium in excess of 300 kilograms in return for natural uranium; or

(c) the modernisation of the Arak reactor based on the agreed conceptual design and, subsequently, on the agreed final design of such reactor.

2. The competent authority granting an authorisation in accordance with paragraph 1 shall ensure the following:

(a) all activities are undertaken strictly in accordance with the JCPOA;

(b) rights to verify the end-use and end-use location of any supplied item have been obtained from Iran and can be exercised effectively.

3. The Member State concerned shall notify the other Member States and the Commission of its intention to grant an authorisation under this Article at least ten days prior to the authorisation.

Article 4a

1. It shall be prohibited to sell, supply, transfer or export, directly or indirectly, the goods and technology listed in Annex III or any other item that the Member State determines could contribute to the devel opment of nuclear weapon delivery systems, whether or not originating in the Union, to any Iranian person, entity or body or for use in Iran. 02012R0267 — EN — 18.01.2017 — 022.003 — 12

▼M24 2. Annex III shall list the items, including goods and technology, contained in the Missile Technology Control Regime list.

Article 4b

It shall be prohibited:

(a) to provide, directly or indirectly, technical assistance or brokering services related to the goods and technology listed in Annex III, or related to the provision, manufacture, maintenance and use of goods listed in Annex III, to any Iranian person, entity or body or for use in Iran;

(b) to provide financing or financial assistance related to the goods and technology listed in Annex III, including in particular grants, loans and export credit insurance for any sale, supply, transfer or export of such items, or for any provision of related technical assistance or brokering services, directly or indirectly, to any Iranian person, entity or body, or for use in Iran;

(c) to enter into any arrangement with an Iranian person, entity or body, or any person or entity acting on their behalf or at their direction, including the acceptance of loans or credit made by such person, entity or body, that would enable such person, entity or body to participate in or increase its participation, be that independently or as part of a joint venture or other partnership, in commercial activities involving technologies listed in Annex III.

Article 4c

It shall be prohibited to purchase, import or transport from Iran, directly or indirectly, the goods and technology listed in Annex III whether the item concerned originates in Iran or not.

Article 5

It shall be prohibited:

(a) to provide technical assistance, brokering services and other services related to the goods and technology listed in the Common Military List of the European Union (‘Common Military List’), and to the provision, manufacture, maintenance and use of goods and tech nology on that list, directly or indirectly to any Iranian person, entity or body or for use in Iran;

(b) to provide financing or financial assistance related to the goods and technology listed in the Common Military List, including in particular grants, loans and export credit insurance for any sale, supply, transfer or export of such items, or for any provision of related technical assistance or brokering services, directly or indi rectly, to any Iranian person, entity or body, or for use in Iran. 02012R0267 — EN — 18.01.2017 — 022.003 — 13

▼M24 (c) to enter into any arrangement for the participation or increase in participation in any Iranian person, entity or body engaged in the manufacture of goods or technology listed in the Common Military List, be that independently or as part of a joint venture or other partnership. This shall include the making of loans or credit to such a person, entity or body.

______

Article 10d

1. A prior authorisation shall be required for:

(a) the sale, supply, transfer or export of the software listed in Annex VIIA, to any Iranian person, entity or body or for use in Iran.

(b) the provision of technical assistance or brokering services related to the software listed in Annex VIIA or related to the provision, manu facture, maintenance and use of such items, to any Iranian person, entity or body, or for use in Iran;

(c) the provision of financing or financial assistance related to the software listed in Annex VIIA, including in particular grants, loans and export credit insurance for any sale, supply, transfer or export of such items, or for any provision of related technical assistance or brokering services to any Iranian person, entity or body, or for use in Iran.

2. The competent authorities shall not grant any authorisation under this Article if:

(a) they have reasonable grounds to determine that the sale, supply, transfer or export of the software is or may be intended for use in connection with the following:

(i) reprocessing- or enrichment-related, heavy water-related, or other nuclear-related activities inconsistent with the JCPOA;

(ii) Iran's military or ballistic missile programme; or

(iii) the direct or indirect benefit of the Iranian Revolutionary Guard Corps;

(b) contracts for delivery of such items or assistance do not include appropriate end-user guarantees.

3. The Member State concerned shall notify the other Member States and the Commission of its intention to grant an authorisation under this Article at least ten days prior to granting the authorisation.

4. Where a competent authority refuses to grant an authorisation, or annuls, suspends, substantively modifies or revokes an authorisation in accordance with this Article, the Member State concerned shall notify the other Member States, the Commission and the High Representative thereof and share the relevant information with them. 02012R0267 — EN — 18.01.2017 — 022.003 — 14

▼M24 5. Before a competent authority of a Member State grants an auth orisation in accordance with this Article for a transaction which is essentially identical to a transaction which is the subject of a still valid denial issued by another Member State or by other Member States, it shall first consult the Member State or Member States which issued the denial. If, following such consultations, the Member State concerned decides to grant an authorisation, it shall inform the other Member States, the Commission and the High Representative thereof, providing all relevant information to explain the decision.

______

Article 15a

1. A prior authorisation shall be required for:

(a) the sale, supply, transfer or export of graphite and raw or semi- finished metals as listed in Annex VIIB, to any Iranian person, entity or body or for use in Iran;

(b) the provision of technical assistance or brokering services related to graphite and raw or semi-finished metals listed in Annex VIIB or related to the provision, manufacture, maintenance and use of such items, to any Iranian person, entity or body, or for use in Iran;

(c) the provision of financing or financial assistance related to graphite and raw or semi-finished metals listed in Annex VIIB, including in particular grants, loans and export credit insurance for any sale, supply, transfer or export of such items, or for any provision of related technical assistance or brokering services to any Iranian person, entity or body, or for use in Iran.

2. The competent authorities shall not grant any authorisation under this Article if:

(a) they have reasonable grounds to determine that the sale, supply, transfer or export of the graphite and raw or semi-finished metals is or may be intended for use in connection with the following:

(i) reprocessing- or enrichment-related, heavy water-related, or other nuclear related activities inconsistent with the JCPOA;

(ii) Iran's military or ballistic missile programme; or

(iii) the direct or indirect benefit of the Iranian Revolutionary Guard Corps;

(b) contracts for delivery of such items or assistance do not include appropriate end-user guarantees.

▼M24 4. Where a competent authority refuses to grant an authorisation, or annuls, suspends, substantively modifies or revokes an authorisation in accordance with this Article, the Member State concerned shall notify the other Member States, the Commission and the High Representative thereof and share the relevant information with them.

5. Before a competent authority of a Member State grants an auth orisation in accordance with this Article for a transaction which is essentially identical to a transaction which is the subject of a still valid denial issued by another Member State or by other Member States, it shall first consult the Member State or Member States which issued the denial. If, following such consultations, the Member State concerned decides to grant an authorisation, it shall inform the other Member States, the Commission and the High Representative thereof, providing all relevant information to explain the decision.

6. The provisions in paragraphs 1 to 3 shall not apply in relation to the goods listed in Annexes I, II and III or in relation to Annex I to Regulation (EC) No 428/2009.

______

▼B

CHAPTER III RESTRICTIONS ON FINANCING OF CERTAIN ENTREPRISES ▼M24 ______

▼B

CHAPTER IV FREEZING OF FUNDS AND ECONOMIC RESOURCES

Article 23

1. All funds and economic resources belonging to, owned, held or controlled by the persons, entities and bodies listed in Annex VIII shall be frozen. Annex VIII includes the persons, entities and bodies designated by the United Nations Security Council or by the Sanctions Committee in accordance with paragraph 12 of UNSCR 1737 (2006), paragraph 7 of UNSCR 1803 (2008) or paragraph 11, 12 or 19 of UNSCR 1929 (2010).

2. All funds and economic resources belonging to, owned, held or controlled by the persons, entities and bodies listed in Annex IX shall be frozen. Annex IX shall include the natural and legal persons, entities and bodies who, in accordance with Article 20(1)(b) and (c) of Council Decision 2010/413/CFSP, have been identified as:

(a) being engaged in, directly associated with, or providing support for Iran's proliferation-sensitive nuclear activities or the development of nuclear weapon delivery systems by Iran, including through involvement in the procurement of prohibited goods and tech nology, or being owned or controlled by such a person, entity or body, including through illicit means, or acting on their behalf or at their direction; 02012R0267 — EN — 18.01.2017 — 022.003 — 16

▼M11 (b) being a natural or legal person, entity or body that has evaded or violated, or assisted a listed person, entity or body to evade or violate, the provisions of this Regulation, Council Decision 2010/413/CFSP or UNSCR 1737 (2006), UNSCR 1747 (2007), UNSCR 1803 (2008) and UNSCR 1929 (2010);

(c) being a member of the Islamic Revolutionary Guard Corps (IRGC) or a legal person, entity or body owned or controlled by the IRGC or by one or more of its members, or a natural or legal person, entity or body acting on their behalf, or a natural or legal person, entity or body providing insurance or other essential services to IRGC, or to entities owned or controlled by them or acting on their behalf;

▼M7 (d) being other persons, entities or bodies that provide support, such as material, logistical or financial support, to the Government of Iran and entities owned or controlled by them, or persons and entities associated with them;

▼M11 (e) being a legal person, entity or body owned or controlled by the Islamic Republic of Iran Shipping Lines (IRISL), or a natural or legal person, entity or body acting on its behalf, or a natural or legal person, entity or body providing insurance or other essential services to IRISL, or to entities owned or controlled by it or acting on its behalf.

▼B Pursuant to the obligation to freeze the funds and economic resources of IRISL and of designated entities owned or controlled by IRISL, it shall be prohibited to load and unload cargoes on and from vessels owned or chartered by IRISL or by such entities in ports of Member States.

The obligation to freeze the funds and economic resources of IRISL and of designated entities owned or controlled by IRISL shall not require the impounding or detention of vessels owned by such entities or the cargoes carried by them insofar as such cargoes belong to third parties, nor does it require the detention of the crew contracted by them.

3. No funds or economic resources shall be made available, directly or indirectly, to or for the benefit of the natural or legal persons, entities or bodies listed in Annexes VIII and IX or.

▼M24 4. Without prejudice to the derogations provided for in Articles 24, 25, 26, 27, 28, 28a, 28b and 29, it shall be prohibited to supply specialised financial messaging services, which are used to exchange financial data, to the natural or legal persons, entities or bodies listed in Annexes VIII and IX.

▼B 5. Annexes VIII and IX shall include the grounds for listing of listed persons, entities and bodies, as provided by the Security Council or by the Sanctions Committee.

6. Annexes VIII and IX shall also include, where available, information necessary to identify the natural or legal persons, entities and bodies concerned, as provided by the Security Council or by the Sanctions Committee. With regard to natural persons, such information may include names including aliases, date and place of birth, nationality, passport and ID card numbers, gender, adress, if known, 02012R0267 — EN — 18.01.2017 — 022.003 — 17

▼B and function or profession. With regard to legal persons, entities and bodies, such information may include names, place and date of regis tration, registration number and place of business. With regard to airlines and shipping companies, Annexes VIII and IX shall also include, where available, information necessary to identify each vessel or aircraft belonging to a listed company such as the original regis tration number or name. Annexes VIII and IX shall also include the date of designation.

▼M24 Article 23a

1. All funds and economic resources belonging to, owned, held or controlled by the persons, entities and bodies listed in Annex XIII shall be frozen. Annex XIII includes the natural and legal persons, entities and bodies designated by the UN Security Council in accordance with paragraph 6(c) of Annex B to UNSCR 2231 (2015).

2. All funds and economic resources belonging to, owned, held or controlled by the persons, entities and bodies listed in Annex XIV shall be frozen. Annex XIV shall include the natural and legal persons, entities and bodies who, in accordance with Article 20(1)(e) of Council Decision 2010/413/CFSP, have been identified as:

(a) being engaged in, directly associated with, or provided support for, Iran's proliferation-sensitive nuclear activities undertaken contrary to Iran's commitments in the JCPOA or the development of nuclear weapon delivery systems by Iran, including through the involvement in procurement of prohibited items, goods, equipment, materials and technology specified in the statement set out in Annex B to UNSCR 2231 (2015), Decision 2010/413/CFSP or the Annexes to this Regu lation;

(b) assisting designated persons or entities in evading or acting incon sistently with the JCPOA, UNSCR 2231 (2015), Decision 2010/413/CFSP or this Regulation;

(d) being a legal person, entity or body owned or controlled by designated persons or entities.

3. No funds or economic resources shall be made available, directly or indirectly, to or for the benefit of the natural or legal persons, entities or bodies listed in Annexes XIII and XIV.

4. Without prejudice to the derogations provided for in Articles 24, 25, 26, 27, 28, 28a, 28b or 29, it shall be prohibited to supply specialised financial messaging services, which are used to exchange financial data, to the natural or legal persons, entities or bodies listed in Annexes XIII and XIV.

5. Annexes XIII and XIV shall include the grounds for listing of listed natural or legal persons, entities or bodies. 02012R0267 — EN — 18.01.2017 — 022.003 — 18

▼M24 6. Annexes XIII and XIV shall also include, where available, the information necessary to identify the natural or legal persons, entities or bodies concerned. With regard to natural persons, such information may include names, including aliases, date and place of birth, nationality, passport and identity card numbers, gender, address if known, and function or profession. With regard to legal persons, entities or bodies, such information may include names, place and date of registration, registration number and place of business. Annexes XIII and XIV shall also include the date of designation.

Article 24

By way of derogation from Article 23 or Article 23a, the competent authorities may authorise the release of certain frozen funds or economic resources, provided that the following conditions are met:

(a) the funds or economic resources are the subject of a judicial, admin istrative or arbitral lien established before the date on which the person, entity or body referred to in Article 23 or Article 23a has been designated by the Sanctions Committee, the UN Security Council or the Council or of a judicial, administrative or arbitral judgment rendered prior to that date;

(b) the funds or economic resources will be used exclusively to satisfy claims secured by such a lien or recognised as valid in such a judgment, within the limits set by applicable laws and regulations governing the rights of persons having such claims;

(d) recognising the lien or judgment is not contrary to public policy in the Member State concerned; and

(e) where Article 23(1) or Article 23a(1) applies, the UN Security Council has been notified by the Member State of the lien or judgment.

Article 25

By way of derogation from Article 23 or Article 23a and provided that a payment by a person, entity or body listed in Annexes VIII, IX, XIII or XIV is due under a contract or agreement that was concluded by, or an obligation that arose for the person, entity or body concerned, before the date on which that person, entity or body had been designated by the Sanctions Committee, the UN Security Council or by the Council, the competent authorities may authorise, under such conditions as they deem appropriate, the release of certain frozen funds or economic resources, provided that the following conditions are met:

(a) the competent authority concerned has determined that:

(i) the funds or economic resources shall be used for a payment by a person, entity or body listed in Annexes VIII, IX, XIII or XIV; 02012R0267 — EN — 18.01.2017 — 022.003 — 19

▼M24 (ii) the payment will not contribute to an activity prohibited under this Regulation. If the payment serves as consideration for a trade activity that has already been performed and the competent authority of another Member State had given prior confirmation that the activity was not prohibited at the time it was performed, it shall be deemed, prima facie, that the payment will not contribute to a prohibited activity; and

(iii) the payment is not in breach of Article 23(3) or Article 23a(3); and

(b) where Article 23(1) or Article 23a(1) applies, the Member State concerned has notified the UN Security Council of that deter mination and its intention to grant an authorisation, and the UN Security Council has not objected to that course of action within ten working days of notification.

Article 26

By way of derogation from Article 23 or Article 23a, the competent authorities may authorise the release of certain frozen funds or economic resources, or the making available of certain funds or economic resources, under such conditions as they deem appropriate, provided that the following conditions are met:

(a) the competent authority concerned has determined that the funds or economic resources concerned are:

(i) necessary to satisfy the basic needs of natural or legal persons, entities or bodies listed in Annexes VIII, IX, XIII or XIV and their dependent family members of such natural persons, including payments for foodstuffs, rent or mortgage, medicines and medical treatment, taxes, insurance premiums, and public utility charges;

(ii) intended exclusively for payment of reasonable professional fees and reimbursement of incurred expenses associated with the provision of legal services; or

(iii) intended exclusively for payment of fees or service charges for routine holding or maintenance of frozen funds or economic resources.

(b) where the authorisation concerns a person, entity or body listed in Annex XIII, the Member State concerned has notified the UN Security Council of the determination referred to in point (a) and its intention to grant an authorisation, and the UN Security Council has not objected to that course of action within five working days of notification.

Article 27

By way of derogation from Article 23(2) and (3) or Article 23a(2) and (3), the competent authorities may authorise the release of certain frozen funds or economic resources or the making available of certain funds or economic resources, under such conditions as they deem appropriate, after having determined that the funds or economic resources concerned are to be paid into or from an account of a diplomatic mission or consular post or an international organisation enjoying immunities in accordance with international law, insofar as such payments are intended to be used for official purposes of the diplomatic mission or consular post or international organisation. 02012R0267 — EN — 18.01.2017 — 022.003 — 20

▼M24 Article 28

By way of derogation from Article 23 or Article 23a, the competent authorities may authorise the release of certain frozen funds or economic resources or the making available of certain funds or economic resources, after having determined that the funds or economic resources concerned are necessary for extraordinary expenses provided that, where the authorisation concerns a person, entity or body listed in Annex XIII, the UN Security Council has been notified of that determination by the Member State concerned and the determination has been approved by the UN Security Council.

Article 28a

By way of derogation from Article 23(2) and (3) or Article 23a(2) and (3), the competent authorities may authorise, under such conditions as they deem appropriate, the release of certain frozen funds or economic resources or the making available of certain funds or economic resources, after having determined that the funds or economic resources concerned are necessary for activities directly related to equipment referred to in paragraph 2(c), subparagraph 1 of Annex B to UNSCR 2231 (2015) for light water reactors.

Article 28b

(a) the competent authority concerned has determined that the funds or economic resources concerned are:

(i) necessary for the civil nuclear cooperation projects described in Annex III of the JCPOA;

(ii) necessary for activities directly related to the items specified in Articles 2a and 3a, or to any other activity required for the implementation of the JCPOA; and

(b) where the authorisation concerns a person, entity or body listed in Annex XIII, the UN Security Council has been notified of that determination by the Member State concerned and the determination has been approved by the UN Security Council.

Article 29

1. Article 23(3) or Article 23a(3) shall not prevent the crediting of the frozen accounts by financial or credit institutions that receive funds transferred by third parties to the account of a listed person, entity or body, provided that any additions to such accounts shall also be frozen. The financial or credit institution shall inform the competent authorities about such transactions without delay.

2. Provided that any such interest or other earnings and payments are frozen in accordance with Article 23(1) or (2) or Article 23a(1) or (2), Article 23(3) or Article 23a(3) shall not apply to the addition to frozen accounts of: 02012R0267 — EN — 18.01.2017 — 022.003 — 21

▼M24 (a) interest or other earnings on those accounts; or

(b) payments due under contracts, agreements or obligations that were concluded or arose before the date on which the person, entity or body referred to in Article 23 or Article 23a has been designated by the Sanctions Committee, the UN Security Council or by the Council.

▼B

CHAPTER V

RESTRICTIONS ON TRANSFERS OF FUNDS AND ON FINANCIAL SERVICES ▼M24 ______

▼M7 ______

▼M24 ______

▼B

CHAPTER VI RESTRICTIONS ON TRANSPORT ▼M24 Article 36

The person providing advance information as determined in the relevant provisions concerning summary declarations as well as customs declar ations in Regulation (EEC) No 2913/92 and in Regulation (EEC) No 2454/93 shall also present any authorisations if required by this Regu lation.

Article 37

1. The provision of bunkering or ship supply services, or any other servicing of vessels, to vessels owned or controlled, directly or indi rectly, by an Iranian person, entity or body shall be prohibited where the providers of the service have information, including from the competent customs authorities on the basis of the advance information referred to in Article 36, that provides reasonable grounds to determine that the vessels carry goods covered by the Common Military List or goods whose supply, sale, transfer or export is prohibited under this Regu lation, unless the provision of such services is necessary for humani tarian and safety purposes.

2. The provision of engineering and maintenance services to cargo aircraft owned or controlled, directly or indirectly, by an Iranian person, entity or body shall be prohibited, where the providers of the service have information, including from the competent customs authorities on the basis of the advance information referred to in Article 36, that provides reasonable grounds to determine that the cargo aircraft carry goods covered by the Common Military List or goods the supply, sale, transfer or export of which is prohibited under this Regulation, unless the provision of such services is necessary for humanitarian and safety purposes. 02012R0267 — EN — 18.01.2017 — 022.003 — 22

▼M24 3. The prohibitions in paragraphs 1 and 2 of this Article shall apply until the cargo has been inspected and, where necessary, seized or disposed of, as the case may be.

Any seizure and disposal may, in accordance with national legislation or the decision of a competent authority, be carried out at the expense of the importer or be recovered from any other person or entity responsible for the attempted illicit supply, sale, transfer or export.

______

▼B

CHAPTER VII GENERAL AND FINAL PROVISIONS

Article 38

1. No claims in connection with any contract or transaction the performance of which has been affected, directly or indirectly, in whole or in part, by the measures imposed under this Regulation, including claims for indemnity or any other claim of this type, such as a claim for compensation or a claim under a guarantee, notably a claim for extension or payment of a bond, guarantee or indemnity, particularly a financial guarantee or financial indemnity, of whatever form, shall be satisfied, if they are made by:

▼M24 (a) designated persons, entities or bodies listed in Annexes VIII, IX, XIII and XIV;

▼B (b) any other Iranian person, entity or body, including the Iranian government;

(c) any person, entity or body acting through or on behalf of one of the persons, entities or bodies referred to in points (a) and (b).

2. The performance of a contract or transaction shall be regarded as having been affected by the measures imposed under this Regulation where the existence or content of the claim results directly or indirectly from those measures.

3. In any proceedings for the enforcement of a claim, the onus of proving that satisfying the claim is not prohibited by paragraph 1 shall be on the person seeking the enforcement of that claim.

4. This Article is without prejudice to the right of the persons, entities and bodies referred to in paragraph 1 to judicial review of the legality of the non-performance of contractual obligations in accordance with this Regulation.

▼M24 ______

▼B

Article 40

1. Without prejudice to the applicable rules concerning reporting, confidentiality and professional secrecy, natural and legal persons, entities and bodies shall: 02012R0267 — EN — 18.01.2017 — 022.003 — 23

▼M24 (a) supply immediately any information which would facilitate compliance with this Regulation, such as information on accounts and amounts frozen in accordance with Article 23 or 23a, to the competent authorities of the Member States where they are resident or located, and shall transmit such information, directly or through the Member States, to the Commission;

▼B (b) cooperate with the competent authorities in any verification of this information.

2. Any additional information received directly by the Commission shall be made available to the Member State concerned.

3. Any information provided or received in accordance with this Article shall be used only for the purposes for which it was provided or received.

▼M24 Article 41

It shall be prohibited to participate, knowingly and intentionally, in activities the object or effect of which is to circumvent the measures in Article 2a, 2b, 2c, 2d, 3a, 3b, 3c, 3d, 4a, 4b, 5, 10d, 15a, 23, 23a and 37 of this Regulation.

▼B

Article 42

1. The freezing of funds and economic resources or the refusal to make funds or economic resources available, carried out in good faith on the basis that such action is in accordance with this Regulation, shall not give rise to liability of any kind on the part of the natural or legal person, entity or body implementing it, or its directors or employees, unless it is proved that the funds and economic resources were frozen or withheld as a result of negligence.

2. The measures set out in the present Regulation shall not give rise to liability of any kind on the part of the natural or legal persons, entities or bodies concerned, if they did not know, and had no reasonable cause to suspect, that their actions would infringe these prohibitions.

▼M24 ______

______

▼B

Article 44

1. The Commission and Member States shall inform each other of the measures taken under this Regulation and share any other relevant information at their disposal in connection with this Regulation at three- monthly intervals, in particular information

▼M24 (a) in respect of funds frozen under Articles 23 and 23a and auth orisations granted under Articles 24, 25, 26, 27, 28, 28a and 28b;

▼B (b) in respect of violations and enforcement problems and judgments issued by national courts. 02012R0267 — EN — 18.01.2017 — 022.003 — 24

▼B 2. The Member States shall immediately inform each other and the Commission of any other relevant information at their disposal which might affect the effective implementation of this Regulation.

▼M24 Article 45

The Commission shall amend Annexes I, II, III, VIIA, VIIB and X on the basis of information supplied by Member States.

Article 46

1. Where the UN Security Council lists a natural or legal person, entity or body, the Council shall include such natural or legal person, entity or body in Annex VIII.

2. Where the Council decides to subject a natural or legal person, entity or body to the measures referred to in Article 23(2) and (3), it shall amend Annex IX accordingly.

3. Where the Council decides to subject a natural or legal person, entity or body to the measures referred to in Article 23a(2) and (3), it shall amend Annex XIV accordingly.

4. The Council shall communicate its decision, including the grounds for listing, to the natural or legal person, entity or body referred to in paragraphs 1 to 3, either directly, if the address is known, or through the publication of a notice, providing such natural or legal person, entity or body with an opportunity to present observations.

5. Where observations are submitted, or where substantial new evidence is presented, the Council shall review its decision and inform the natural or legal person, entity or body accordingly.

6. Where the United Nations decides to delist a natural or legal person, entity or body, or to amend the identifying data of a listed natural or legal person, entity or body, the Council shall amend Annex VIII or XIII accordingly.

7. The lists in Annexes IX and XIV shall be reviewed in regular intervals and at least every 12 months.

▼B

Article 47

1. Member States shall lay down the rules on penalties applicable to infringements of this Regulation and shall take all measures necessary to ensure that they are implemented. The penalties provided for shall be effective, proportionate and dissuasive.

2. Member States shall notify the Commission of those rules without delay after the entry into force of this Regulation and shall notify it of any subsequent amendment. 02012R0267 — EN — 18.01.2017 — 022.003 — 25

▼B Article 48

1. Member States shall designate the competent authorities referred to in this Regulation and identify them on the websites listed in Annex X. Member States shall notify the Commission of any changes in the addresses of their websites listed in Annex X.

2. Member States shall notify the Commission of their competent authorities, including the contact details of those competent authorities, without delay after the entry into force of this Regulation, and shall notify it of any subsequent amendment.

3. Where this Regulation sets out a requirement to notify, inform or otherwise communicate with the Commission, the address and other contact details to be used for such communication shall be those indicated in Annex X.

Article 49

This Regulation shall apply:

(a) within the territory of the Union, including its airspace;

(b) on board any aircraft or any vessel under the jurisdiction of a Member State;

(d) to any legal person, entity or body, inside or outside the territory of the Union, which is incorporated or constituted under the law of a Member State;

(e) to any legal person, entity or body in respect of any business done in whole or in part within the Union.

Article 50

Regulation (EU) No 961/2010 is hereby repealed. References to the repealed regulation shall be construed as references to this Regulation.

Article 51

This Regulation shall enter into force on the day of its publication in the Official Journal of the European Union.

This Regulation shall be binding in its entirety and directly applicable in all Member States. 02012R0267 — EN — 18.01.2017 — 022.003 — 26

)

Metal vessels, or major shop-fabricated especially designed Metal vessels, or parts therefor, major shop-fabricated or as defined in paragraph 1.1. reactor nuclear of a core to contain the prepared defined in paragraph 1.8. as below. internals reactor above, as well relevant of regardless vessels reactor nuclear 1.2 covers Item EXPLANATORY NOTE pressure rating and includes pressure vessels reactor and calandrias. The vessel head is covered by part 1.2. reactor shop-fabricated item as a major vessel. of a reactor sustaining fission chain reaction. items the includes basically reactor” “nuclear A EXPLANATORY NOTE vessel, the equipment which to the reactor directly within or attached the level of power in controls core, and the components which normally coolant of the contact with or control the primary contain or come in direct core. EXPORTS reactor The export of the whole set of major items within this boundary will take place only in accordance with the procedures of the Guide lines. Those individual items within defined this functionally boundary which will be exported only in accordance with the procedures of the Guidelines are right to in paragraphs 1.2. the to 1.11. listed to itself The Government reserves within the apply functionally the procedures of Guidelines to other items defined boundary Nuclear Suppliers Group's control list as in INFCIRC/254/Rev.12/Part 1 ( Nuclear Suppliers Group's as control in INFCIRC/254/Rev.12/Partlist 1 Nuclear reactor vessels reactor Nuclear

TLB1.2 TLB1.1 Complete nuclear reactors nuclear TLB1.1 Complete ANNEX I CATEGORY 0 — NUCLEAR MATERIALS, FACILITIES, AND EQUIPMENT MATERIALS,FACILITIES, AND NUCLEAR— CATEGORY 0

transit of dual-use items vessel head for a reactor pressure vessel, specially designed vessel head pressure vessel, specially for a reactor or to prepared contain the core of a “nuclear reactor”; components therefor, as follows: as components therefor, 0A001 “Nuclear reactors” and specially designed or prepared equipment and equipment prepared or designed specially and reactors” 0A001 “Nuclear 0A001.a reactors”; “Nuclear TLB1.1 capable of operation so a controlled self- as to maintain reactors Nuclear 0A001.b including parts therefor, Metal vessels, or the reactor major shop-fabricated 2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and brokering exports, transfer, of control the for 5 Community 2009 of regime a up May 2009 setting The corresponding Council No 428/ in systems, equipment Regulation (EC) and components identified as 0A Systems, Equipment and Components and Equipment 0A Systems, M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 27

Zirconium metal tubes or zirconium alloy tubes (or assemblies of tubes) tubes assemblies tubes or zirconium alloy (or Zirconium metal as cladding designed for use as fuel especially in a reactor or prepared kg. in paragraph 1.1. defined above, and exceeding 10 in quantities N.B.: tubes see 1.8. tubes see 1.5. pressure For calandria For zirconium tubes for alloy tubes or zirconium EXPLANATORY metal NOTE Zirconium of hafnium relation zirconium in which the consist of reactor use in a nuclear less than 1:500 is typically to zirconium parts by weight Tubes which are especially designed or prepared to contain both fuel elements both fuel contain to prepared designed or especially are Tubes which as defined in paragraph 1.1. above. coolant in a reactor and the primary to designed channels fuel of parts are tubes Pressure EXPLANATORY NOTE operate at elevated pressure, sometimes in excess of 5 MPa. Manipulative equipment especially designed or prepared for inserting or inserting designed for or prepared Manipulative equipment especially in paragraph 1.1. as defined above. reactor in a nuclear removing fuel on-load of capable are above noted items The EXPLANATORY NOTE operation or at employing sophisticated positioning technically or alignment fueling operations such to allow complex as those in off-load which features direct viewing of or access to the fuel is not normally available. Especially designed Especially or prepared rods, support or suspension therefor, structures in a process fission rod guide the mechanisms or tubes to control rod drive as defined nuclear reactor in paragraph 1.1. above. Nuclear reactor control rods and equipment and rods control reactor Nuclear Nuclear fuel cladding fuel Nuclear Nuclear reactor pressure tubes pressure reactor Nuclear Nuclear reactor fuel charging and discharging machines discharging and charging fuel reactor Nuclear TLB1.4 TLB1.6 TLB1.5 TLB1.3

0A001.h. process in a “nuclear reactor”, support process in or suspension reactor”, therefor, a “nuclear structures mechanisms and rod guide tubes; rod drive N.B.: 0A001.e. For zirconium pressure tubes see and for calandria tubes see and the primary coolant in a “nuclear reactor”; reactor”; “nuclear a coolant in primary and the specially designed or prepared for use as fuel cladding in a “nuclear kg; exceeding 10 and in quantities reactor”, removing fuel in a “nuclear reactor”; reactor”; “nuclear a in removing fuel 0A001.f Zirconium metal tubes or zirconium alloy tubes (or assembles of tubes) of assembles (or tubes alloy zirconium or tubes metal 0A001.f Zirconium 0A001.e Pressure tubes specially designed or prepared to contain both fuel elements fuel both contain to prepared or designed specially tubes 0A001.e Pressure 0A001.c Manipulative equipment specially designed or prepared for inserting or inserting for prepared or designed specially equipment 0A001.c Manipulative 0A001.d the control of fission designed Control or prepared for rods specially

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 28

Pumps or circulators especially designed the especially Pumps for circulating or prepared or circulators primary coolant as for nuclear reactors defined in paragraph 1.1. above. EXPLANATORY designed pumps NOTE: Especially or prepared or circu lators include pumps for for gas-cooled water-cooled reactors, circulators and pumps and mechanical liquid-metal-cooled for electromagnetic reactors, This equipment may include reactors. pumps sealed or multi- with elaborate sealed systems to prevent leakage of primary coolant, canned-driven pumps, and pumps mass systems. This definition encompasses pumps with inertial components) 1 of Subsection NB (Class Division I, III, to Section certified Society of Mechanical Engineers (ASME) Code, the American or equivalent standards. “Nuclear reactor internals” especially designed or prepared for use in a nuclear for designed prepared or especially internals” reactor “Nuclear as defined in paragraph 1.1 above. reactor This includes, for example, support baffles, shields, tubes, thermal channels, calandria fuel core, the columns for core grid plates, and plates. diffuser structures major are internals” reactor “Nuclear EXPLANATORY NOTE supporting such as functions more one or which have vessel reactor a within coolant flow, providing primary alignment, directing the core, maintaining fuel radiation shields for the vessel, and reactor guiding in-core instrumentation. (a) Steam generators especially designed or prepared for the primary, or inter primary, the designed for or prepared especially generators Steam (a) as defined in 1.1 paragraph of a nuclear reactor above. mediate, coolant circuit (b) Other heat exchangers especially designed or prepared for use in the primary coolant circuit of a nuclear as reactor defined in paragraph 1.1 above. prepared or designed especially are generators Steam EXPLANATORY NOTE gener steam for water to the feed in the reactor the heat generated to transfer coolant loop which an intermediate for reactor of a fast the case ation. In Primary coolant pumps or circulators or pumps coolant Primary Nuclear reactor internals reactor Nuclear Heat exchangers Heat TLB1.7 TLB1.8 TLB1.9

of the reactor, e.g., the emergency cooling system or the decay heat cooling system. mediate, coolant of circuit a “nuclear reactor”; of primary coolant a circuit “nuclear reactor”; “nuclear reactor”, including “nuclear reactor”, support columns for the core, fuel channels, calandria tubes, thermal shields, baffles, core grid plates, and diffuser plates; the primary coolant of “nuclear reactors”; reactors”; coolant of “nuclear the primary Technical Note: In 0A001.h. ‘nuclear reactor internals’ means any major structure within a which has one or more functions such as supporting core, the vessel reactor providing flow, coolant primary directing alignment, maintaining fuel and instrumentation. vessel, guiding reactor in-core for the radiation shields systems supporting the for exchangers heat control not does Note: 0A001.i. 1. Steam generators specially designed or prepared for the primary, or inter or primary, the for prepared or designed specially generators 1. Steam 2. Other heat exchangers specially designed or prepared for use in the 0A001.i Heat exchangers as follows: as exchangers 0A001.i Heat 0A001.h ‘Nuclear reactor internals’ specially designed or prepared for use in a in use for prepared or designed specially internals’ reactor 0A001.h ‘Nuclear 0A001.g Coolant pumps specially designed or circulators or prepared for circulating

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 29

per second or more. Ex-

neutrons per cm neutrons per

per second to 10

2 Especially designed or prepared neutron detectors for determining neutron flux determining for neutron detectors prepared designed or Especially levels within the core of a as defined reactor in paragraph 1.1. above. ex- and in-core encompasses entry this of scope The EXPLANATORY NOTE core detectors which measure flux levels in a large range, typically from 10 special fissionable material and equipment, special fissionable material other than analytical instruments, especially designed or prepared therefor core refers to those instruments outside the core of a reactor as defined in to those instruments outside the core of a reactor refers core shielding. biological the within located 1.1. above, but paragraph is also present, the In steam generator is in a circuit. the gas- intermediate heat to a secondary a heat exchanger to cooled may be reactor, transfer utilized gas loop drives a gas that turbine. The scope this entry does not of control for include heat exchangers for the supporting e.g., systems of the reactor, the cooling system. decay heat the or cooling system emergency neutrons per cm neutrons per “External thermal shields” designed thermal shields” especially “External or prepared for use in a nuclear as defined in paragraph 1.1 reduction of heat loss and for reactor also for containment vessel protection. structures major are shields” thermal “External EXPLANATORY NOTE placed over the reactor vessel which reduce heat loss from the reactor and within the containment vessel. reduce temperature Neutron detectors Neutron External thermal shields thermal External TLB5 uranium, depleted uranium or of isotopes of natural the separation for Plants TLB1.10 TLB1.11

reactor” for the reduction reactor” of heat loss and also for the containment vessel protection. or “special fissile materials”, and designed materials”, specially or or “special fissile prepared equipment follows: as and components therefor, Technical Note: In 0A001.k. thermal shields’ means ‘external major structures placed over which reduce heat loss from the reactor vessel the reactor and reduce temperature within the containment vessel. levels within the core of a “nuclear reactor”; 0B001 of isotopes the “depleted uranium” uranium”, separation of “natural Plant for 0A001.j Neutron detectors specially designed or prepared for determining neutron flux neutron determining for prepared or designed specially detectors 0A001.j Neutron 0A001.k ‘External thermal shields’ specially designed or prepared for use in a “nuclear “nuclear a in use for prepared or designed specially shields’ thermal 0A001.k ‘External

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 30

gas and

or prepared for use in gas centrifuges or prepared featuring at least three separate channels, of which two are connected to scoops extending from the rotor axis towards periphery of chamber. Also contained within the vacuum a number of environment are critical items which do not rotate and which although they are especially out nor designed are they to of unique fabricated fabricate are not difficult A however centrifuge facility materials. requires a large number of these components, so that quantities can provide an important indication of end use. INTRODUCTORY NOTE of between cylinder(s) thin-walled normally consists of a The gas centrifuge contained in a vacuum environment and spun mm diameter at mm and 650 75 axis m/s or more with its central speed high peripheral of the order 300 In order to achieve high of construction for the speed vertical. the materials and rotor components the rotating to density ratio have to be of a high strength assembly, and individual components, hence its have to be manufactured the unbalance. in order to to other minimize In contrast very close tolerances centrifuges, the gas centrifuge for uranium enrichment by is characterized and a baffle(s) disc-shaped rotating a chamber rotor the having within stationary tube arrangement for feeding and extracting the UF 5.1. Gas centrifuges and assemblies and components especially designed especially components and assemblies and centrifuges Gas 5.1.

TLB5 TLB5.1

m and a “specific tensile strength” greater than 7,62 × strength” greater than 7,62 tensile m and a “specific

or m;

4 than 3,18 × 10 × than 3,18 more; more; 10 prepared for gas separation process, centrifuge as follows: 3. “Fibrous or filamentary materials” with a “specific modulus” of more of modulus” “specific a with materials” filamentary or 3. “Fibrous 1. Gas centrifuges; 1. Gas Technical Note: In 0B001.b. means ‘high ratio material’ strength-to-density any of the follow ing: or GPa 1,95 of strength tensile ultimate an of capable steel 1. Maraging or GPa 0,46 of strength tensile ultimate an of capable alloys 2. Aluminium “depleted uranium”, or “special fissile materials”, as follows: as materials”, fissile “special or “depleted uranium”, plant; separation centrifuge 1. Gas plant; separation diffusion 2. Gaseous plant; separation 3. Aerodynamic plant; separation exchange 4. Chemical plant; separation 5. Ion-exchange plant; separation isotope “laser” vapour 6. Atomic plant; separation isotope “laser” 7. Molecular plant; separation 8. Plasma plant; separation magnetic 9. Electro 0B001.a Plant specially designed for separating isotopes of “natural uranium”, “natural of isotopes separating for designed specially 0B001.a Plant 0B001.b designed or and components, specially and assemblies centrifuges Gas

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 31

gas circulation within the main separation chamber of chamber separation main within the gas circulation

the rotor tube, and from one manufactured of the high strength to density ratio materials described in the EXPLANATORY NOTE to this Section. Disc-shaped components of between 75 mm and 650 mm diameter especially mm diameter mm and 650 Disc-shaped components of between 75 order tube, in rotor centrifuge the be mounted inside to prepared designed or chamber and, the main separation in some chamber from the take-off to isolate the UF cases, to assist Thin-walled or a number cylinders, cylinders, of interconnected thin-walled Thin-walled from one manufactured or more of the high strength to density materials ratio EXPLANATORY interconnected, in the described Section. If NOTE to this as described in bellows or rings by joined flexible together are cylinders the and end baffle(s) section 5.1.1.(c) following. with an internal The rotor is fitted form. caps, as described in section 5.1.1.(d) in final following, if and (e) assembled. However the complete assembly may be delivered only partly mm thickness of 12 with cylinders thin-walled designed prepared or Especially mm, and from manufactured mm and 650 of between 75 or less, a diameter one or more of the high described in the strength to density materials ratio Section. this to EXPLANATORY NOTE Components especially designed or prepared to give localized support to the to give localized Componentsdesigned or prepared especially a number tube or to of rotor tubes. join together rotor The bellows is a short mm and of between 75 mm or less, a diameter thickness 3 of wall cylinder 650 mm, having a convolute, and manufactured from one of the high strength described in the EXPLANATORY materials to density NOTE to this ratio Section. TLB5.1.1 Rotating components TLB5.1.1 Rotating TLB5.1.1c (c) Rings or Bellows: or Rings TLB5.1.1c (c) TLB5.1.1d (d) Baffles: TLB5.1.1d (d) TLB5.1.1b (b) Rotor tubes: Rotor TLB5.1.1b (b) between 75 mm and 650 mm and designed support to to give local a mm and 650 between 75 rotor tube or to join a number together, made from ‘high strength-to- materials’; density ratio rotor tube, made from ‘high strength-to-density ratio materials’. rotor tube, made ‘high from materials’. strength-to-density ratio of between 75 mm and 650 mm, made from ‘high strength-to-density mm, made from mm and 650 of between 75 ratio materials’; 0B001.b 0B001.b. 4. of and diameter a mm or less thickness of 3 Rings wall or bellows with a 0B001.b. 5. mounting for inside a mm diameter mm and 650 of between 75 Baffles 0B001.b. 2. assemblies; Complete rotor TLB5.1.1a (a) assemblies: Complete rotor 0B001.b. 3. mm or less, a diameter Rotor tube cylinders with a wall thickness of 12

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 32

2 -resistant 6

; ‘Specific

3 m or greater and a specific ultimate tensile ultimate and a specific m or greater

6 m or greater (‘Specific Modulus’ is the Young's (‘Specific m or greater

4 divided by the specific weight in N/m weight in divided by specific the

material (see EXPLANATORY NOTE to Section 5.2.). The magnet a second couples to top with a pole piece or the cap magnet fitted described in Section 5.1.1.(e). and between outer a relation may be ring-shaped with The magnet a or equal to 1,6:1. may be in The magnet smaller diameter inner annular magnet suspended within a housing containing a damping a UF from be manufactured medium. The housing will within the rotor tube, and in some cases to support, retain or contain as an or to support, retain tube, and in some cases rotor within the strength of 7,62 × 10 strength of 7,62 N/m Modulus in more; more; × specific modulus 10 of 3,18 N/m weight in divided by specific the Ultimate Tensile Strength’ Ultimate Tensile Strength’ is the ultimate tensile strength in N/m 1. Especially designed consisting 1. Especially or prepared bearing assemblies of an

integrated part an element of the upper bearing (top cap) or to carry the rotating elements of the motor and lower bearing (bottom cap), and manu factured from one of the high strength to density described ratio materials in the EXPLANATORY NOTE to this Section. The materials used for centrifuge rotating components include the following: centrifuge used for The materials or 1,95 GPa of strength tensile ultimate an of capable steel (a) Maraging or GPa 0,46 of strength tensile ultimate an of capable alloys (b) Aluminium a having and structures composite in use for suitable materials (c) Filamentary Disc-shaped components of between 75 mm and 650 mm diameter especially mm diameter mm and 650 Disc-shaped components of between 75 tube, and so contain the rotor ends of the to the fit to designed or prepared UF TLB5.1.1 EXPLANATORY NOTE TLB5.1.1 EXPLANATORY TLB5.1.2 Static components TLB5.1.2 Static TLB5.1.1e (e) Top caps/Bottom caps: caps/Bottom Top TLB5.1.1e (e) TLB5.1.2A.1 (a) Magnetic suspension bearings: suspension Magnetic TLB5.1.2A.1 (a) ” containing a damping medium and having the magnet coupling 6

a housing made of or protected by “materials resistant to corrosion by resistant a housing by made of or protected “materials UF with a pole piece or second to the top magnet cap of the rotor; fitted gas centrifuges. a. Bearing assemblies consisting of an annular magnet suspended within suspended magnet annular an of consisting assemblies a. Bearing b. Active magnetic bearings specially designed or prepared for use with use for prepared or designed specially bearings magnetic b. Active ends of a rotor tube, made from ‘high ratio materials’; strength-to-density 0B001.b 0B001.b. 7. Magnetic suspension bearings as follows: as bearings suspension Magnetic 0B001.b. 7. 0B001.b. 6. the to fit mm diameter mm and 650 Top between 75 or bottom caps of

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 33 . In

centrifuges. form having an initial permeability of 0,15 form having permeability an H/m or more, a remanence initial % or more, or an energy than 80 product kJ/m of greater of 98,5 more than one to function for in order power supply unit ruptible (UPS) hour. addition to the usual material properties, it is a prerequisite that the that prerequisite a is it properties, usual material addition to the to axes is limited axes deviation of the magnetic from the geometrical or that homogeneity mm) of the than 0,1 (lower tolerances very small material of the magnet is specially called for. — Designed to keep centred a rotor spinning at 600 Hz or more, and EXPLANATORY NOTE more, or Hz 600 at spinning These bearings usually have the following characteristics: rotor a centred keep to — Designed — power supply and/or to an uninter electrical Associated to a reliable Especially designed or prepared bearings comprising a pivot/cup assembly comprising a bearings prepared designed or Especially with a mounted shaft on damper. The pivot hardened a is normally a steel described bottom cap the to attachment means of a one end with at hemisphere hydrodynamic may however have a other. The shaft 5.1.1.(e) at the in section The indentation bearing attached. cup with in a hemispherical is pellet-shaped one surface. These components to the damper. often supplied separately are Especially designed or prepared cylinders having internally machined or having internally cylinders designed prepared or Especially machined bores. grooves dimensions Typical and extruded helical internally are as follows: 75 mm to 650 mm internal diameter, 10 mm or more wall thickness, typically The grooves than the diameter. are greater length equal to or with the in depth. mm or more and 2 in cross-section rectangular TLB5.1.2c (c) Molecular pumps: Molecular TLB5.1.2c (c) TLB5.1.2b (b) Bearings/Dampers: TLB5.1.2b (b) TLB5.1.2a2 2. Active magnetic bearings especially designed or prepared for use with gas with use for prepared or designed especially bearings magnetic Active TLB5.1.2a2 2. a damper; extruded helical grooves and internally machined bores; grooves and internally extruded helical 0B001.b. 0B001.b. 8. Specially prepared bearings comprising a pivot-cup assembly mounted on mounted assembly pivot-cup a comprising bearings prepared Specially 0B001.b. 8. 0B001.b. 9. Molecular pumps comprised of cylinders having internally machined or machined internally having cylinders of comprised pumps Molecular 0B001.b. 9.

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 34

gas from

Frequency changers (also known as converters or inverters) especially inverters) known or Frequency changers (also converters as 5.1.2.(d), or under defined as stators supply motor to prepared designed or parts, components and sub-assemblies of such frequency changers having all following characteristics: of the and Hz or greater; 1. A multiphase frequency output of 600 %). 0,2 than better control frequency (with stability 2. High Especially designed Especially or prepared tubes for the extraction of UF within the rotor tube by a Pitot tube action (that is, with an aperture facing with an aperture is, tube action (that tube by a Pitot the rotor within example by bending tube, for within the rotor gas flow into the circumferential the end disposed of a radially tube) and capable of being fixed to the central system. gas extraction Especially designed or prepared ring-shaped stators for high speed multiphase for stators ring-shaped designed prepared or Especially synchronous for motors a operation within reluctance) (or AC hysteresis and a power 40 of Hz or greater VA or 600 vacuum a frequency of at windings low of multi-phase on may consist a laminated The stators greater. mm thick or less. typically 2,0 of thin layers core comprised loss iron Componentsdesigned to especially or prepared contain the rotor tube The housing assembly of a gas centrifuge. consists of a rigid cylinder mm with precision machined ends to locate the wall thickness up to 30 mounting. ends The machined for flanges more one or and with bearings to are parallel each other and perpendicular to the cylinder's longitudinal axis to within 0,05 or less. The housing degrees may also be a honeycomb assemblies. rotor to accommodate several type structure 5.2.5. Frequency changers Frequency 5.2.5. TLB5.2.5 TLB5.1.2f (f) Scoops: TLB5.1.2f (f) TLB5.1.2e (e) Centrifuge housing/recipients: Centrifuge TLB5.1.2e (e) TLB5.1.2d (d) Motor stators: Motor TLB5.1.2d (d) and gas from within the rotor tube by a Pitot tube action

and capable of being fixed to the central gas extraction system; gas extraction central the to being fixed and capable of centrifuge, consisting of a rigid cylinder of wall thickness up to 30 mm thickness up of wall to 30 cylinder consisting of a rigid centrifuge, other and perpen to each parallel machined ends are with precision that 0,05 longitudinal axis to within less; cylinder's degrees or to the dicular extraction of UF motors for synchronous motors for operation within a vacuum at a frequency of Hz or more and a power of 40 VA or more; 600 prepared to supply enrichment, having for gas centrifuge motor stators and all of the following specially designed characteristics, components therefor: greater; or Hz 600 of output frequency multiphase a. A b. High stability (with frequency control better than 0,2 %); 0,2 than better control frequency (with stability b. High 0B001.b. 13. Frequency changers (converters or inverters) specially designed or designed specially inverters) or (converters changers Frequency 0B001.b. 13. 0B001.b. 11. Centrifuge housing/recipients to contain the rotor tube assembly of a gas a of assembly tube rotor the contain to housing/recipients Centrifuge 0B001.b. 11. 0B001.b. the designed tubes for Scoops or prepared consisting of specially 12. 0B001.b. 10. Ring-shaped motor stators for multiphase AC hysteresis (or reluctance)

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 35

(see

, with an inside , with 6

-resistant materials (see , and with a discharge , and with a 6

per minute or more of UF (see EXPLANATORY NOTE to section 5.4), and

3 6

gaseous streams of an individual gas centrifuge. individual gas an of gaseous streams

or tails UF or tails or protected by materials resistant to corrosion by UF corrosion to resistant by materials protected or diameter of 10 to 160 mm, especially designed or prepared for use in main for designed prepared mm, or especially of 10 to 160 diameter plants. enrichment systems of gas centrifuge or auxiliary — 100 nm, a thickness of 5 mm or less, and for tubular forms, a diameter tubular mm or less, and for nm, a thickness of 5 — 100 resistant materials polymer or ceramic mm or less, made of metallic, of 25 to corrosion by UF Especially designed or prepared hermetically sealed vessels for containing the for vessels sealed hermetically prepared designed or Especially by UF or protected of made barrier, gaseous diffusion (a) Shut-off valves especially designed or prepared to act on the feed, product feed, the on act to prepared or designed especially valves (a) Shut-off pressure of up to 500 kPa, designed for long-term operation in the UF operation in the up long-term to 500 of kPa, designed for pressure EXPLANATORY NOTE to section 5.4). section to EXPLANATORY NOTE designed Especially or prepared compressors gas blowers with a suction m 1 of volume capacity environment, as well as separate assemblies of such of compressors and assemblies gas separate as environment, as well blowers. These compressors and gas of 10:1 blowers have a pressure ratio or less and are made to of, or UF resistant protected by, materials (b) Bellows-sealed valves, manual or automated, shut-off or control, made of made control, or shut-off automated, or manual valves, (b) Bellows-sealed (a) Especially designed or prepared thin, porous filters, with a pore size of 10 of size pore a with filters, porous thin, prepared or designed (a) Especially EXPLANATORY NOTE to section 5.4). section to EXPLANATORY NOTE EXPLANATORY NOTE Typical especially designed or prepared valves include valves, bellow-sealed fast acting closure-types, fast acting valves and others. Gaseous diffusion barriers and barrier materials barrier and barriers diffusion Gaseous Diffuser housings Diffuser blowers gas and Compressors 5.2.3 Special shut-off and control valves control and shut-off Special 5.2.3 TLB5.3.2 TLB5.3.3 TLB5.2.3 TLB5.3.1a /min

3 ”, with an inside diameter of ”, with an inside diameter 6

” with a pore size of ” with a pore 10 size to 6

gaseous streams of an individual gas centrifuge; gas individual an of gaseous streams

”; ”; 6 6

, discharge pressure up to 500 , discharge pressure kPa and having pressure a 6

“materials resistant to “materials corrosion by UF product or tails UF product or tails 10 mm to 160 mm, specially designed or prepared for use in main or auxiliary systems of gas centrifuge enrichment plants; b. valves, by shut-off or control, made of Bellows-sealed protected a. Shut-off valves specially designed or prepared to act on the feed, the on act to prepared or designed specially valves a. Shut-off “materials resistant to corrosion by UF 100 nm, a thickness of 5 mm or less, and, forms, a for tubular nm, a thickness of 5 100 mm or less; of 25 diameter or more of UF or more ratio of 10:1 or less, and made of or protected by “materials resistant to resistant of 10:1 by or less, and ratio made of or protected “materials corrosion by UF corrosion by UF 1. Gaseous diffusion barriers made of porous metallic, polymer or ceramic or polymer metallic, porous of made diffusion separation process, as follows: barriers diffusion 1. Gaseous for gaseous designed or prepared and components, specially Equipment 0B001.c 0B001.c 3. Compressors or gas blowers with a suction volume capacity of 1 m 1 of capacity volume suction a with blowers gas or Compressors 0B001.c 3. 0B001.c 2. to housings Gaseous resistant diffuser made of or protected by “materials 0B001.b. 14. Shut-off and control valves as follows: as valves control and Shut-off 0B001.b. 14.

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 36

- 6

and having a knife- and having a

, and with one or more tangential inlets. The inlets. tangential more one or , and with 6

per minute.

. Such seals are normally designed for a buffer gas in-leakage rate of less of rate gas in-leakage buffer a designed for normally are . Such seals gaseous diffusion of systems main and auxiliary in installation , for 6 6

Especially designed or prepared heat exchangers made of or protected by UF protected heat exchangers made of or designed or prepared Especially The thereof. and assemblies nozzles separation prepared designed or Especially of radius having channels curved a of slit-shaped, consist nozzles separation mm, to resistant corrosion by UF curvature less than 1 both ends. or either appendages at nozzletype equipped with be may tubes Especially designed or prepared bellows-sealed valves, manual or automated, valves, bellows-sealed prepared designed or Especially to corrosion by resistant or control, made by of or protected shut-off materials UF edge within the nozzle that separates the gas flowing through the the nozzle into separates edge within the nozzle that two fractions. Especially designed or prepared vortex tubes and assemblies thereof. The thereof. vortex tubes and assemblies prepared designed or Especially made of or protected by or tapered, materials cylindrical vortex tubes are resistant to corrosion by UF resistant materials (see EXPLANATORY NOTE to section 5.4), and intended for a leakage pressure change rate of less than 10 Pa per hour under a pressure difference of 100 kPa. than 1 000 cm 000 than 1 enrichment plants. Especially designed Especially or prepared vacuum seals, with seal feed and seal exhaust connections, the shaft connecting for sealing the compressor or gas blower rotor with the driver motor so as to seal against ensure a in-leaking of reliable air into the inner chamber of the compressor or gas blower which is filled with UF Heat exchangers for cooling UF cooling for exchangers Heat Separation nozzles Separation Special shut-off and control valves control and shut-off Special Vortex tubes Vortex Rotary shaft seals shaft Rotary TLB5.3.5 TLB5.5.1 TLB5.4.4 TLB5.5.2 TLB5.3.4 , and /min.;

3 ”; 6

” and with one or more tangential more one or and with ” 6

”, and designed for a leakage pressure rate of less than 10 less Pa per of rate pressure leakage a ”, and designed for 6

hour under a pressure differential of 100 kPa of differential pressure hour under a having a knife-edge contained within the nozzle which separates the gas the nozzle which separates contained within the having knife-edge a flowing through the nozzle into two streams; by UF or protected by “materials resistant to corrosion by resistant UF by or protected “materials to mm, corrosion by resistant UF radius of curvature less than 1 inlets; “materials resistant to corrosion by UF designed for a buffer gas in-leakage rate of less than 1 000 cm 000 than 1 of less rate gas in-leakage a buffer designed for 1. Separation nozzles consisting of slit-shaped, curved channels having a having channels curved aerodynamic separation process, as follows: slit-shaped, of consisting nozzles 1. Separation Equipment and components, specially designed or prepared for prepared or designed specially components, and Equipment 0B001.c 5. to corrosion resistant by exchangers “materials made of or protected Heat 0B001.c 6. or control, made of valves, manual or automated, shut-off Bellows-sealed 0B001.c 4. Rotary shaft seals for compressors or blowers in specified 0B001.c.3. and 0B001.d 0B001.d 2. or conical tubes, Cylindrical (vortex tubes), made of or protected by

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 37 / 6

/carrier gas 6

, for containing vortex , for 6

gas streams and of the following: having gas streams all

mass spectrometers/Ion sources mass spectrometers/Ion

a resolution of better than 1 part in 320; of better a resolution by alloys; % or more weight, or nickel-chrome a nickel content of 60 (hydrogen or helium) mixture. helium) (hydrogen or Rotary shaft seals feed and seal with seal seals, shaft designed prepared rotary or Especially exhaust connections, the shaft connecting for sealing the compressor rotor or seal motor so as to a reliable ensure with the driver the gas blower rotor against out-leakage of process or gas or seal gas in-leakage of air into the inner chamber of the compressor or with gas blower a UF which is filled Compressors and gas blowers gas blowers made of or compressors or designed or prepared Especially UF the by corrosion to resistant by materials protected housings, element designed separation made of or or prepared Especially corrosion by UF to resistant by materials protected of taking on-line capable spectrometers mass designed prepared or Especially UF samples from carrier gas mixture. EXPLANATORY NOTE The feed gas enters the vortex tube tangentially at EXPLANATORY the vortex tube tangentially gas enters NOTE The feed numerous positions along the at tangential vanes one end or or through swirl periphery of the tube. by designed heat exchangers made of or protected Especially or prepared materials resistant to corrosion by UF tubes or separation nozzles. tubes or separation 1. and Capable ions having of measuring of 320 mass units or greater atomic with alloys nickel-copper nickel, by protected or of constructed sources 2. Ion sources; ionization bombardment 3. Electron analysis. isotopic for suitable system collector a 4. Having UF housings element Separation Heat exchangers for gas cooling gas for exchangers Heat TLB5.5.3 TLB5.5.4 TLB5.5.6 TLB5.5.5 TLB5.5.10 ”, with a diameter a with ”, 6

”, ”, and rotary shaft seals therefor; ” to contain vortex tubes or separation nozzles; 6 6

”; 6

by UF mm or more; of 40 to corrosion by UF or protected by “materials resistant to corrosion by UF corrosion to resistant by “materials protected or to corrosion by UF 0B001.d 4. to corrosion resistant by exchangers “materials made of or protected Heat 0B001.d 3. Compressors resistant or gas blowers made of or protected by “materials 0B001.d 6. or control, made of valves, manual or automated, shut-off Bellows-sealed 0B001.d 5. resistant housings, element by Separation made of or protected “materials

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 38

from from

. 6

cold traps capable of freezing out UF capable of freezing cold traps

/carrier gas separation systems 153 K (–120 °C) or less, or less, or °C) (–120 153 K or less, carrier gas, or 6

carrier gas (hydrogen or helium). UF the reduce to designed are systems These EXPLANATORY NOTE Especially designed or prepared process systems for separating UF separating for systems process prepared designed or Especially content in the carrier gas to 1 ppm and or less equipment may incorporate gas to 1 content in the carrier such as: of temperatures of capable cryoseparators and exchangers heat (a) Cryogenic °C) (–120 K 153 of temperatures of capable units refrigeration (b) Cryogenic UF of separation the for units tube vortex or nozzle (c) Separation (d) UF designed for or prepared especially contactors Liquid-liquid centrifugal using exchange uranium enrichment the chemical process. Such contactors and and aqueous of the organic dispersion streams to achieve use rotation to resistance the phases. For corrosion to separate force then centrifugal made normally are contactors solutions, the hydrochloric acid concentrated hydrocarbon (such as fluorinated materials of or protected by suitable plastic is contactors of the centrifugal time residence or glass. The stage polymers) normally designed to be 30 seconds or less. Countercurrent liquid-liquid exchange columns having mechanical power using the enrichment uranium for prepared designed or input, especially chemical exchange process. For corrosion resistance to concentrated hydro chloric acid solutions, these columns and their internals are normally made of (such hydrocarbon as fluorinated or protected by materials suitable plastic polymers) or glass. The stage residence time of the columns is normally less. 30 seconds or be designed to UF TLB5.6.2 Liquid-liquid centrifugal contactors (Chemical exchange) (Chemical contactors centrifugal TLB5.6.2 Liquid-liquid TLB5.6.1 Liquid-liquid exchange columns (Chemical exchange) (Chemical columns exchange TLB5.6.1 Liquid-liquid TLB5.5.12 from

; 6

from carrier gas (hydrogen from carrier or helium)

content or less, including: content or

cold traps capable of freezing out UF of freezing capable cold traps

of 153K (–120 °C) or less; of 153K (–120 °C) (–120 or less; carrier gas; to 1 ppm UF to 1 a. Cryogenic heat exchangers and capable of temperatures cryoseparators b. Cryogenic refrigeration units capable UF of of temperatures separation of the for 153 units K tube vortex or nozzle c. Separation of 30 hydrochloric to concentrated seconds time or less and resistant such as fluor materials plastic by suitable or protected (e.g. made of acid inated hydrocarbon polymers or glass); seconds or less and resistant to concentrated hydrochloric seconds to concentrated acid (e.g. made or less and resistant such hydro as fluorinated by materials of or protected suitable plastic glass) or carbon polymers d. UF 1. Fast-exchange liquid-liquid pulse columns with stage residence time of 30 follows: as process, exchange separation of time residence stage with columns pulse liquid-liquid 1. Fast-exchange 0B001.e 2. Fast-exchange liquid-liquid centrifugal contactors with stage residence stage with contactors centrifugal liquid-liquid Fast-exchange 0B001.e 2. 0B001.e chemical for designed or prepared Equipment and components, specially 0B001.d 7. Process systems for separating UF separating for systems Process 0B001.d 7.

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 39

from the organic into stream an aqueous

+4 out of the organic stream, adjusting the acid concen out of the organic stream,

for taking the U tration and feeding to reduction the cells. electrochemical uranium from one valence state to another for uranium enrichment using uranium enrichment for to another state one valence uranium from with process in contact materials exchange process. The cell the chemical hydrochloric acid to concentrated solutions must be corrosion resistant solutions. solution, evaporation and/or other equipment to accomplish solution pH solution, evaporation and/or other feeding to for devices transfer and pumps other and control, or adjustment A major design concern is to avoid reduction cells. the electrochemical ions. Consequently, metal certain with aqueous stream the of contamination constructed of is the system stream, the process with contact in those parts for glass, fluor (such as materials by suitable equipment made of or protected sulfone, and resinimpregnated polyether ocarbon polymers, polyphenyl sulfate, graphite). Especially designed or prepared systems for producing for high-purity uranium systems designed or prepared Especially chloride feed solutions for chemical exchange uranium isotope separation plants. EXPLANATORY NOTE These systems consist of solvent extraction solvent of consist systems These EXPLANATORY NOTE the U stripping equipment for (a) Especially designed or prepared electrochemical reduction cells to reduce to cells reduction electrochemical prepared or designed (a) Especially to designed be must compartment cathodic cell The EXPLANATORY NOTE To keep state. higher valence the of uranium to its prevent re-oxidation may have an impervious uranium in the cathodic compartment, cell The exchange cation special material. diaphragm membrane constructed of solid conductor cathode consists of a suitable such as graphite. TLB5.6.4 Feed preparation systems (Chemical exchange) (Chemical systems preparation TLB5.6.4 Feed TLB5.6.3a Uranium reduction systems and equipment (Chemical exchange) (Chemical equipment and systems reduction TLB5.6.3a Uranium TLB5.6.3b (b) designed Especially or prepared systems at the product end of the cascade from the

+4 ;

+3 to U

+4 or U

+6 solution consisting of dissolution, solvent extraction and/or ion exchange dissolution, solvent extraction solution consisting of uranium reducing the for cells and electrolytic purification equipment for U organic stream and, those organic stream in contact with for parts the process stream, (e.g. glass, fluorocarbon by materials made of or protected suitable polymers, polyphenyl sulphate, polyether sulfone and resin-impregnated graphite); solutions, for reduction of uranium from one valence state to another; state one valence uranium from reduction of solutions, for 0B001.e 5. Feed preparation systems for producing high purity uranium chloride uranium purity high producing for systems preparation Feed 0B001.e 5. 0B001.e 4. Electrochemical reduction cells feed equipment to take U take to equipment feed cells reduction Electrochemical 0B001.e 4. 0B001.e 3. Electrochemical reduction cells resistant to concentrated hydrochloric acid hydrochloric concentrated to resistant cells reduction Electrochemical 0B001.e 3.

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 40 into the

for return

+4 +4 to U

+3 . These systems produce systems . These

+3 to U

+4 include glass, fluorinated hydrocarbon include glass, fluorinated or U

+6 +3

to the uranium isotope separation to the uranium isotope cascade in the chemical exchange separation enrichment process. as: such equipment incorporate may systems These EXPLANATORY NOTE (a) Equipment for contacting chlorine and oxygen with the aqueous effluent the isotope U equipment from separation and the resultant extracting polymers, polyphenyl sulfate or polyether sulfone plastic-lined and resin- plastic-lined sulfone or polyether polymers, polyphenylsulfate 5.6.5. Uranium 1 June 2013 39 - - NSG Part graphite. impregnated uranium chloride solutions having of metallic only per million a few parts impurities such as chromium, iron, vanadium, molybdenum and other bivalent of construction for portions of the cations. Materials or higher multi-valent system processing high-purity U EXPLANATORY NOTE These systems consist of dissolution, solvent dissolution, of consist systems These EXPLANATORY NOTE and electrolytic purification ion exchange equipment for and/or extraction cells for reducing the uranium U returning from the product stripped organic stream end of the cascade, (b) Equipment water from hydrochloric acid that separates so that the and water the at process the to be reintroduced may acid hydrochloric concentrated the proper locations. Fast-reacting ion-exchange resins or adsorbents especially designed or exchange process, including ion using the enrichment uranium for prepared active which the in structures pellicular and/or resins, porous macroreticular chemical exchange groups are limited to a coating on the surface of an inactive porous support and structure, other composite in any structures suitable form including or particles fibres. These ion exchange resins/ mm or less and must be chemically of 0,2 adsorbents have diameters as physically hydrochloric acid solutions to concentrated as well resistant strong enough so as not to degrade in the exchange columns. The resins/ uranium isotope designed very fast to achieve especially adsorbents are and are than 10 seconds) less of half-time (exchange rate exchange kinetics °C) to 473 K in the range of 373 K a temperature (100 capable of operating at (200 °C). Especially designed or prepared systems for oxidation of U for systems designed prepared or Especially TLB5.6.6 Fast-reacting ion exchange resins/adsorbents (Ion exchange) (Ion resins/adsorbents exchange ion TLB5.6.6 Fast-reacting ; TLB5.6.5 Uranium oxidation systems (Chemical exchange) (Chemical systems oxidation Uranium ; TLB5.6.5

+4 to U

+3 resins in which the active chemical exchange groups are limited to a exchange limited groups chemical in which are the active resins and porous of an inactive other support structure, coating on the surface fibres, or including in any form, particles suitable composite structures hydrochloric to concentrated mm or less, resistant of 0,2 with diameters acid and designed of less than 10 to have an exchange half-time rate range of 373 in the seconds K and capable of operating at temperatures (100 °C) to 473 K (200 °C); separation process, as follows: as process, separation macro-reticulated porous or pellicular resins, ion-exchange reacting 1. Fast 0B001.f Equipment and components, specially designed or prepared for ion-exchange for prepared or designed specially components, and 0B001.f Equipment 0B001.e 6. Uranium oxidation systems for oxidation of U of oxidation for systems oxidation Uranium 0B001.e 6.

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 41

(a) Especially designed or prepared chemical or electrochemical reduction or electrochemical designed chemical Especially or prepared (a) reducing used regeneration of the systems for chemical agent(s) in ion prepared designed or Especially (b) cascades. enrichment exchange uranium oxidation of the chemical systems for regeneration or electrochemical chemical cascades. ion exchange uranium enrichment used in oxidizing agent(s) Cylindrical columns greater than 1 000 mm in for containing diameter and 000 Cylindrical columns than greater 1 designed especially exchange resin/adsorbent, ion of supporting packed beds for uranium enrichment using or prepared the ion exchange process. These or fluorocarbon (such as titanium by made of or protected columns materials are to corrosion by concentrated hydrochloric acid solutions resistant and plastics) in the range of 373 capable of operating at a temperature K (100 are °C) to 473 K (200 °C) and pressures above 0,7 MPa. vapour based methods) handling uranium, molten for designed molten systems or prepared Especially vapour enrichment or use uranium alloys or metal in laser for especially designed or prepared components therefore. may systems handling metal uranium liquid The EXPLANATORY NOTE The crucibles and the crucibles. cooling equipment consist of crucibles for and other parts of this system that come into contact with molten uranium, vapour by are made of or protected molten uranium alloys or metal Especially designed or prepared uranium metal vaporization systems for use in for systems vaporization uranium metal designed or prepared Especially laser enrichment. and guns beam electron contain may systems These EXPLANATORY NOTE kW on or greater) the target are designed to achieve a delivered power (1 sufficient to generate uranium metal vapour at a rate required for the laser enrichment function. TLB5.6.8 Ion exchange reflux systems (Ion exchange) (Ion systems reflux exchange TLB5.6.8 Ion TLB5.6.7 Ion exchange columns (Ion exchange) (Ion columns exchange TLB5.6.7 Ion TLB5.7.2 Liquid or vapour uranium metal handling systems and components (atomic components and systems handling metal uranium vapour or TLB5.7.2 Liquid TLB5.7.1 vapour based Uranium vaporization systems (atomic methods) reduction systems) for regeneration of the chemical reducing or of the chemical reduction systems) for regeneration cascades; ion exchange enrichment used in oxidizing agents 1 000 mm, made of or protected by materials resistant to concentrated resistant mm, made of or protected by materials 000 1 and capable of or fluorocarbon plastics) hydrochloric acid (e.g. titanium °C) to 473 K in the range of 373 K (100 temperatures operating at (200 °C) and pressures above 0,7 MPa; prepared for handling molten uranium, molten uranium alloys or uranium metal vapour for use in laser enrichment, and specially designed components therefor; power of 1 kW or more on the target for use in laser enrichment; use in laser kW for on or more the target power of 1 N.B.: SEE ALSO 2A225. ALSO N.B.: SEE separation processes using atomic vapour laser isotope separation, as follows: as isotope separation, vapour laser using atomic processes separation 1. Uranium metal vaporization systems designed to achieve a delivered 0B001.f 3. Ion exchange reflux systems (chemical or electrochemical oxidation or oxidation electrochemical or (chemical systems reflux exchange Ion 0B001.f 3. 0B001.f 2. Ion exchange columns (cylindrical) with a diameter greater than greater diameter a with (cylindrical) columns exchange Ion 0B001.f 2. 0B001.g 2. Liquid or vapour uranium metal handling systems specially designed or designed specially systems handling metal uranium vapour or Liquid 0B001.g 2. 0B001.g laser-based for prepared Equipment and components, designed or specially

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 42

Lasers or laser systems especially designed or prepared for the separation of uranium isotopes. in importance of components laser and lasers The EXPLANATORY NOTE laser-based enrichment processes include those identified in INFCIRC/254/ Part 2 — (as amended). The system laser typically contains both optical and Especially designed or prepared cylindrical or rectangular vessels for or rectangular designed Especially cylindrical or prepared beam gun, vapour source, containing the electron and the uranium metal the collectors. and ‘product’ ‘tails’ elec for ports of multiplicity housings have These EXPLANATORY NOTE trical and water feed-throughs, laser beam windows, vacuum pump have diagnostics and monitoring. They and instrumentation connections internal of refurbishment allow to opening closure and provisions for components. methods) for assemblies designed collector or prepared ‘product’ and Especially ‘tails’ in liquid or solid form. uranium metal or of made are assemblies these Components for EXPLANATORY NOTE to protected by resistant the heat and materials corrosion of uranium metal and may include tantalum) or graphite vapour or liquid (such as yttria-coated exchangers and feed-throughs, heat collector ‘gutters’, pipes, valves, fittings, or other separation methods. plates for magnetic, electrostatic materials of suitable corrosion and heat resistance. Suitable materials may earth graphite, graphite coated with other rare include tantalum, yttria-coated thereof. mixtures or amended)) 2 — (as INFCIRC/254/Part oxides (see Separator module housings (atomic vapour based methods) based vapour (atomic housings module Separator TLB5.7.4 TLB5.7.3 Uranium (atomic vapour and collector assemblies metal ‘product’ ‘tails’ based TLB5.7.13 Laser systems TLB5.7.13 Laser separation of uranium isotopes with a spectrum frequency stabilisation frequency spectrum a with isotopes uranium of separation for operation over extended periods of time; containing the uranium metal vapour source, the electron beam gun and vapour electron source, the containing the uranium metal collectors; the product and tails form, made of or protected by materials resistant to form, made the of or resistant heat and protected by corrosion materials or graphite vapour or liquid, such of uranium metal yttria-coated as tantalum; N.B.: SEE ALSO 6A005 AND 6A205. AND 6A005 ALSO N.B.: SEE 0B001.g the designed for prepared systems specially or or “laser” “Lasers” 5. 0B001.g 4. Separator module housings (cylindrical or rectangular vessels) for vessels) rectangular or (cylindrical housings module Separator 0B001.g 4. 0B001.g 3. Product and tails collector assemblies for uranium metal in liquid or solid or liquid in metal uranium for assemblies collector tails and Product 0B001.g 3.

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 43 /carrier gas mixtures, 6

. 6

environment. The components of

environment. .

/ UF 5

lasers or excimer lasers and a multi-pass optical cell. and carrier gas to 150 K (–123 °C) or less and which are or less °C) gas to 150 K (–123 and carrier

) solid The material. product may collectors consist impact, of or filter, /carrier gas compressors (molecular based methods)

5 6

Lasers or laser systems for both methods require spectrum frequency stabil ization for operation over extended periods of time. Especially designed or prepared components or devices for collecting uranium components collecting designed or devices for or prepared Especially product material or uranium tails material following illumination with laser light. separ isotope laser molecular of example one In EXPLANATORY NOTE enriched uranium pentafluoride to serve collect ation, the product collectors (UF made of or gas are come into contact with process compressors that these corrosion by UF to resistant by materials protected Especially designed cooling supersonic expansion or prepared for nozzles Especially mixtures of UF to UF corrosion resistant UF a in operation long term designed for cyclone-type collectors, or combinations cyclone-type collectors, and thereof, must be corrosion resistant to the UF electronic components for the management of the laser beam (or beams) and beams) beam (or the laser components the management of for electronic the transmission to system for isotope separation chamber. The laser atomic vapour based methods usually consists of tunable dye lasers pumped (e.g., by copper or certain vapour another type of laser lasers based methods system for molecular The may laser lasers). solid-state consist of CO Especially designed or prepared compressors for UF for compressors designed or prepared Especially TLB5.7.7 UF TLB5.7.5 Supersonic expansion nozzles (molecular based methods) based (molecular nozzles expansion TLB5.7.5 Supersonic TLB5.7.6 based (molecular methods) collectors or ‘tails’ ‘Product’ and carrier gas and carrier

”; 6

”, and rotary shaft seals therefor; seals shaft ”, and rotary 6

prepared for collecting uranium material or uranium tails material or uranium tails uranium prepared for collecting material to resistant light, made of “materials with laser following illumination corrosion by UF to 150 K (–123 °C) or less and made from “materials resistant to corrosion resistant °C) or less and “materials made from to 150 K (–123 by UF UF separation processes using molecular laser isotope separation, as follows: as separation, isotope laser using molecular processes separation UF of mixtures cooling for nozzles expansion 1. Supersonic 0B001.h components collector or devices specially designed Product or tails or 2. 0B001.h 3. to corrosion by resistant by Compressors made of or protected “materials 0B001.h laser-based for prepared Equipment and components, designed or specially

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 44

from

cold traps

(solid) to UF

/carrier gas mixture. 6

for subsequent collection in product containers

. The carrier gas may be nitrogen, argon, or other . The carrier 6

are used.

powder to UF powder to

powder may be removed/transferred from the ‘product’ collectors into a collectors ‘product’ the from powder may be removed/transferred /carrier gas separation systems (molecular based methods)

5 6

capable of freezing out capable of freezing UF suitable reaction vessel or (e.g., screw flame reactor reactor, fluidized-bed tower) for fluorination. In both approaches, equipment for storage and of fluorine (or other suitable fluorinating agents) and transfer for collection UF of and transfer gas. carrier gas. EXPLANATORY NOTE These systems may incorporate capable cryoseparators Cryogenic heat exchangers or (a) equipment such as: °C) or less, or (b) Cryogenic refrigeration of 153 of temperatures K (– 120 °C) UF or less, of (c) 153 units capable of temperatures K (–120 or for transfer as feed for additional enrichment. In one approach, or for transfer the fluor may be accomplished within the isotope separation system to ination reaction react and recover directly off the ‘product’ collectors. In another approach, the UF Especially designed or prepared rotary shaft seals, with seal feed and seal with seal seals, shaft designed prepared rotary or Especially connecting compressor rotor the the shaft exhaust connections, sealing for against out-leakage of seal motor so with the driver as to ensure a reliable process gas or in-leakage of air or seal gas into the inner chamber of the with a UF compressor which is filled (gas). the fluorinate to designed are systems These EXPLANATORY NOTE collected UF UF separating for systems process prepared designed or Especially Especially designed or prepared systems for fluorinating UF fluorinating for designed systems or prepared Especially TLB5.7.8 Rotary shaft seals (molecular based methods) based (molecular seals shaft TLB5.7.8 Rotary TLB5.7.12 UF (gas); TLB5.7.9 Fluorination systems (molecular based methods) based (molecular systems Fluorination (gas); TLB5.7.9 ;

from carrier gas (e.g. nitrogen, from carrier argon

(solid) to UF

cold traps capable of freezing out UF of freezing capable cold traps

of 153 K (–120 °C) or less; of 153 K (–120 °C) (–120 or less; or other gas) including: a. Cryogenic heat exchangers and capable of temperatures cryoseparators b. Cryogenic refrigeration units capable of temperatures of 153 K c. UF 0B001.h 5. Process systems for separating UF separating for systems Process 0B001.h 5. 0B001.h 4. Equipment for fluorinating UF fluorinating for Equipment 0B001.h 4.

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 45 lasers or

Especially designed or prepared microwave power sources and antennae for power sources microwave prepared designed or Especially greater characteristics: following having the and ions accelerating producing or than 30 GHz frequency and greater than production. 50 kW mean power output for ion Especially designed radio frequency ion coils for prepared Especially or excitation than of more 100 frequencies kHz and capable of handling than more 40 kW mean power. excimer lasers and a multi-pass optical cell. Lasers or laser systems for both over extended operation for frequency stabilization spectrum methods require periods of time. Especially designed or prepared systems for the generation of uranium plasma the systems for designed or prepared Especially for use in plasma separation plants. Lasers or laser systems especially designed or prepared for the separation of uranium isotopes. in importance of components laser and lasers The EXPLANATORY NOTE laser-based enrichment processes include those identified in INFCIRC/254/Part and elec contains both optical system typically amended). The laser 2 — (as and the beams) beam (or the laser the management of components for tronic atomic system for laser chamber. The separation the isotope to transmission pumped by dye lasers of tunable vapour based methods usually consists lasers). solid-state (e.g., copper or certain vapour another type of laser lasers based methods may consist molecular of CO system for The laser TLB5.8.1 Microwave power sources and antennae and sources power TLB5.8.1 Microwave TLB5.8.2 Ion excitation coils excitation TLB5.8.2 Ion TLB5.7.13 Laser systems TLB5.7.13 Laser ions, with an output frequency greater than 30 GHz and mean power GHz and mean 30 than output greater an frequency ions, with kW; 50 than output greater and capable of handling more than 40 kW mean power; handling than 40 of more and capable separation of uranium isotopes with a spectrum frequency stabilisation frequency spectrum a with isotopes uranium of separation for operation over extended periods of time; separation process, as follows: as process, separation 1. Microwave power sources and antennae for producing or accelerating N.B.: SEE ALSO 6A005 AND 6A205. AND 6A005 ALSO N.B.: SEE 0B001.i Equipment and components, specially designed or prepared for plasma for prepared or designed specially components, and 0B001.i Equipment 0B001.i 2. Radio frequency ion excitation coils for frequencies of more than 100 kHz 100 than more of frequencies for coils excitation ion frequency Radio 0B001.i 2. 0B001.i 3. Uranium plasma generation systems; TLB5.8.3 Uranium plasma generation systems 0B001.h designed for the systems specially prepared or or “laser” “Lasers” 6.

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 46

sources consisting of a vapour source, ionizer, and beam accelerator, such steel, or as graphite, constructed of stainless suitable materials 50 mA or of current ion beam of providing a total copper, and capable greater. Especially designed or prepared ‘product’ and ‘tails’ collector assemblies for assemblies designed collector or prepared ‘product’ and Especially ‘tails’ are made assemblies of or uranium metal in solid form. These collector to protected by resistant the heat and materials corrosion of uranium metal graphite or tantalum. vapor, such as yttria-coated Electromagnetic isotope especially designed separators Electromagnetic or prepared for the and components isotopes, and equipment therefor, uranium of separation including: ion uranium multiple or single prepared or designed Especially sources (a) Ion for use in plasma separation enrichment plants for containing the uranium and “tails” “product” and the coil drive radio-frequency source, plasma collectors. EXPLANATORY NOTE These housings have a multiplicity of feed-throughs, diffusion pump connections ports for electrical and instrumen opening and and monitoring. They have provisions for diagnostics tation closure to of internal components refurbishment allow for and constructed are steel. such as stainless non-magnetic material of a suitable TLB5.8.5 Uranium metal ‘product’ and ‘tails’ collector assemblies assemblies collector ‘tails’ and ‘product’ metal TLB5.8.5 Uranium TLB.5.8.6 Separator module housings Cylindrical vessels especially designed or prepared or designed especially vessels Cylindrical housings module TLB.5.8.6 Separator TLB5.9.1a Electromagnetic isotope separators isotope TLB5.9.1a Electromagnetic made of or protected by materials resistant to the heat and corrosion of resistant by made of or protected materials or tantalum; uranium vapour graphite such as yttria-coated beam accelerator made of suitable non-magnetic materials (e.g. graphite, non-magnetic materials made of suitable beam accelerator stainless steel, or copper) and capable of providing a total ion beam of 50 mA or greater; current source, radio-frequency drive coil and the product and tails collectors and collectors product and tails and the coil drive radio-frequency source, steel); (e.g. stainless a suitable non-magnetic material made of 1. Ion sources, single or multiple, consisting of a vapour source, ioniser, and agnetic separation process, as follows: ioniser, source, vapour a of consisting multiple, or single sources, 1. Ion 0B001.i 5. Product and tails collector assemblies for uranium metal in solid form, solid in metal uranium for assemblies collector tails and Product 0B001.i 5. 0B001.j Equipment and components, specially designed or prepared for electrom for prepared or designed specially components, and 0B001.j Equipment 0B001.i 4. Not used; TLB5.8.4 14 No longer used — since June 2013 0B001.i 6. Separator module housings (cylindrical) for containing the uranium plasma uranium the containing for (cylindrical) housings module Separator 0B001.i 6.

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 47

Especially designed or prepared magnet pole pieces having a diameter greater having diameter magnet pole pieces a designed or prepared Especially within an electromagnetic a constant magnetic field m used to maintain than 2 between adjoining the magnetic field separ and isotope separator to transfer ators. Especially designed or prepared high-voltage power supplies for ion sources, high-voltage power supplies for designed prepared or Especially capable of continuous having of the operation, all following characteristics: and A or greater, of output 1 current V or greater, 000 output voltage of 20 period of 8 hours. % over a time than 0,01 voltage regulation of better Collector plates consisting of two or more slits and consisting pockets of two or more slits especially plates Collector ion uranium depleted and enriched of collection for prepared designed or steel. such or stainless as graphite beams and materials constructed of suitable Especially designed or prepared vacuum housings for uranium electromagnetic designed vacuum or prepared housings uranium electromagnetic Especially for such as stainless constructed of suitable non-magnetic materials separators, and designed steel of 0,1 for operation at pressures Pa or lower. the contain to designed specially are housings The EXPLANATORY NOTE provision for and have liners and water-cooled plates collector sources, ion and reinstal pump removal connections and opening for diffusion and closure lation of these components. TLB5.9.2 High voltage power supplies power voltage TLB5.9.2 High TLB5.9.1c Vacuum housings TLB5.9.1c Vacuum TLB5.9.1b Ion collectors TLB5.9.1b Ion and magnetic materials (e.g. stainless steel) and steel) (e.g. designed stainless magnetic materials to operate at of 0,1 pressures Pa or lower; d. Voltage regulation of better than 0,01 % over a period of 8 hours; than 0,01 d. of better Voltage regulation beams, consisting of two or more slits and pockets suitable and slits made of beams, consisting of two or more steel); (e.g. graphite or stainless non-magnetic materials characteristics: operation; continuous of a. Capable V or greater; 000 b. Output voltage of 20 c. A or greater; of 1 Output current N.B.: SEE ALSO 3A227. ALSO N.B.: SEE 0B001.j 3. Vacuum housings for uranium electromagnetic separators made of non- of made separators electromagnetic uranium for housings Vacuum 0B001.j 3. 0B001.j 4. m; than 2 greater with a diameter Magnet pole pieces TLB5.9.1d Magnet pole pieces 0B001.j 2. plates for collection of enriched Ion or depleted collector uranium ion 0B001.j 5. High voltage power supplies for ion sources, having all of the following the of all having sources, ion for supplies power voltage High 0B001.j 5.

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 48

, , 6 6

to to

6 6

from from

6 6

into containers. into containers.

6 6

to a liquid or solid to a liquid or solid

6 6

from the enrichment process for subsequent upon transfer from the enrichment process for subsequent upon transfer

6 6

including: (a) Feed autoclaves, ovens, or systems used for passing ovens, UF Feed autoclaves, systems used for or including: (a) the enrichment process by compressing and converting UF UF stations used transferring for ‘Product’ or ‘tails’ (d) form; passing ovens, UF Feed autoclaves, systems used for or including: (a) the enrichment process by compressing and converting UF UF stations used transferring for ‘Product’ or ‘tails’ (d) form; Especially designed or prepared high-power, direct current magnet power designed current high-power, or prepared direct Especially continuously of capable the following characteristics: of supplies having all V or greater at a voltage of 100 A or greater producing a current output of 500 % over a period of 8 than 0,01 better or voltage regulation and with a current hours. designed Especially or prepared process systems equipment for enrichment by UF corrosion to resistant by materials protected or of made plants the enrichment process; (b) Desublimers, cold traps or pumps used to remove UF designed Especially or prepared process systems equipment for enrichment by UF corrosion to resistant by materials protected or of made plants the enrichment process; (b) Desublimers, cold traps or pumps used to remove UF heating; (c) Solidification or liquefaction stations used to Solidification remove UF heating; (c) or liquefaction stations used to Solidification remove UF heating; (c) TLB5.9.3 Magnet power supplies power TLB5.9.3 Magnet systems withdrawal tails and systems/product TLB5.2.1 Feed systems withdrawal tails and systems/product TLB5.4.1 Feed to the enrichment

”: 6

and greater at a voltage of 100 V or greater; at a voltage of 100 greater hours. following characteristics: or A 500 of output current a with operation continuous of a. Capable b. Current or voltage regulation better than 0,01 % over a period of 8 b. than Current or 0,01 voltage regulation better N.B.: SEE ALSO 3A226. ALSO N.B.: SEE process; as follows, for isotope separation isotope plant specified in 0B001, as follows, for separation made of or to corrosion by resistant protected by UF “materials 0B002 Specially designed or prepared auxiliary systems, equipment and components, and equipment systems, auxiliary prepared or designed 0B002 Specially 0B001.j 6. Magnet power supplies (high power, direct current) having all of the of all having current) direct power, (high supplies power Magnet 0B001.j 6. 0B002.a Feed autoclaves, ovens or systems used for passing UF passing for used systems or ovens autoclaves, 0B002.a Feed

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 49

, , , 6 6

6 6 6

to to to

6 6 6

from

into containers.

to a liquid or solid

from the enrichment from the enrichment

into containers into containers. 6 6

6 6

to a liquid or solid form; (d) form; liquid or solid to a (d) form; liquid or solid to a

6 6

from the enrichment process for subsequent upon transfer

Especially designed Especially or prepared process systems equipment for enrichment by UF corrosion to resistant by materials protected or of made plants process by compressing and converting UF process by compressing and converting UF including: (a) Feed autoclaves, ovens, or systems used for passing ovens, UF Feed autoclaves, systems used for or including: (a) passing ovens, UF Feed autoclaves, systems used for or including: (a) passing ovens, UF Feed autoclaves, systems used for or including: (a) the enrichment process by compressing and converting UF UF stations used transferring for ‘Product’ or ‘tails’ (d) form; the enrichment process; (b) Desublimers (or cold traps) used to remove UF (or cold traps) Desublimers the enrichment process; (b) used to remove UF (or cold traps) Desublimers the enrichment process; (b) the enrichment process; (b) Desublimers, cold traps or pumps used to remove UF ‘Product’ or ‘tails’ stations used for transferring UF stations used for transferring or ‘tails’ ‘Product’ designed Especially or prepared process systems equipment for enrichment by UF corrosion to resistant by materials protected or of made plants UF stations used for transferring or ‘tails’ ‘Product’ heating; (c) Solidification or liquefaction stations used to Solidification remove UF heating; (c) Especially designed Especially or prepared process systems equipment for enrichment by UF corrosion to resistant by materials protected or of made plants from the enrichment process for subsequent upon Solidifi transfer heating; (c) cation or liquefaction stations used to remove UF from the enrichment process for subsequent upon Solidifi transfer heating; (c) cation or liquefaction stations used to remove UF TLB5.2.1 Feed systems/product and tails withdrawal systems withdrawal tails and systems/product TLB5.2.1 Feed TLB5.5.7 Feed systems/product and tails withdrawal systems withdrawal tails and systems/product TLB5.5.7 Feed TLB5.7.11 Feed systems/product and tails withdrawal systems (molecular based methods) based (molecular systems withdrawal tails and systems/product TLB5.7.11 Feed from the enrichment process

for subsequent upon transfer heating; 0B002.b Desublimers or cold traps, used to remove UF remove to used traps, cold or 0B002.b Desublimers

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 50

, , , 6 6

6 6 6

to to to

6 6 6

from

into containers.

to a liquid or solid

from the enrichment from the enrichment

into containers. into containers. 6 6

6 6

to a liquid or solid form; (d) form; liquid or solid to a (d) form; liquid or solid to a

6 6

from the enrichment process for subsequent upon transfer

process by compressing and converting UF process by compressing and converting UF including: (a) Feed autoclaves, ovens, or systems used for passing ovens, UF Feed autoclaves, systems used for or including: (a) the enrichment process by compressing and converting UF UF stations used transferring for ‘Product’ or ‘tails’ (d) form; passing ovens, UF Feed autoclaves, systems used for or including: (a) passing ovens, UF Feed autoclaves, systems used for or including: (a) the enrichment process; (b) Desublimers, cold traps or pumps used to remove UF designed Especially or prepared process systems equipment for enrichment by UF corrosion to resistant by materials protected or of made plants used to remove UF (or cold traps) Desublimers the enrichment process; (b) used to remove UF (or cold traps) Desublimers the enrichment process; (b) ‘Product’ or ‘tails’ stations used for transferring UF stations used for transferring or ‘tails’ ‘Product’ UF stations used for transferring or ‘tails’ ‘Product’ heating; (c) Solidification or liquefaction stations used to Solidification remove UF heating; (c) designed Especially or prepared process systems equipment for enrichment by UF corrosion to resistant by materials protected or of made plants Especially designed Especially or prepared process systems equipment for enrichment by UF corrosion to resistant by materials protected or of made plants from the enrichment process for subsequent upon Solidifi transfer heating; (c) cation or liquefaction stations used to remove UF from the enrichment process for subsequent upon Solidifi transfer heating; (c) cation or liquefaction stations used to remove UF TLB5.5.7 Feed systems/product and tails withdrawal systems withdrawal tails and systems/product TLB5.5.7 Feed TLB5.4.1 Feed systems/product and tails withdrawal systems withdrawal tails and systems/product TLB5.4.1 Feed TLB5.7.11 Feed systems/product and tails withdrawal systems (molecular based methods) based (molecular systems withdrawal tails and systems/product TLB5.7.11 Feed

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 51

, , , 6

6 6 6

to to to

6 6 6

from from

6 6

into containers. into containers.

6 6

to a liquid or solid to a liquid or solid

6 6

from the enrichment

into containers. 6

to a liquid or solid form; (d) form; liquid or solid to a

from the enrichment process for subsequent upon transfer from the enrichment process for subsequent upon transfer

6 6

process by compressing and converting UF including: (a) Feed autoclaves, ovens, or systems used for passing ovens, UF Feed autoclaves, systems used for or including: (a) the enrichment process by compressing and converting UF UF stations used transferring for ‘Product’ or ‘tails’ (d) form; passing ovens, UF Feed autoclaves, systems used for or including: (a) the enrichment process by compressing and converting UF UF stations used transferring for ‘Product’ or ‘tails’ (d) form; passing ovens, UF Feed autoclaves, systems used for or including: (a) the enrichment process; (b) Desublimers, cold traps or pumps used to remove UF designed Especially or prepared process systems equipment for enrichment by UF corrosion to resistant by materials protected or of made plants the enrichment process; (b) Desublimers, cold traps or pumps used to remove UF designed Especially or prepared process systems equipment for enrichment by UF corrosion to resistant by materials protected or of made plants used to remove UF (or cold traps) Desublimers the enrichment process; (b) ‘Product’ or ‘tails’ stations used for transferring UF stations used for transferring or ‘tails’ ‘Product’ heating; (c) Solidification or liquefaction stations used to Solidification remove UF heating; (c) or liquefaction stations used to Solidification remove UF heating; (c) Especially designed Especially or prepared process systems equipment for enrichment by UF corrosion to resistant by materials protected or of made plants from the enrichment process for subsequent upon Solidifi transfer heating; (c) cation or liquefaction stations used to remove UF TLB5.4.1 Feed systems/product and tails withdrawal systems withdrawal tails and systems/product TLB5.4.1 Feed systems withdrawal tails and systems/product TLB5.5.7 Feed into containers; TLB5.2.1 systems withdrawal Feed systems/product and tails

0B002.c Product and tails stations for transferring UF transferring for stations tails and 0B002.c Product

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 52

, , , 6

6 6 6

to to to

6 6 6

from from

6 6

into containers. into containers.

6 6

to a liquid or solid to a liquid or solid

6 6

from the enrichment

into containers. 6

to a liquid or solid form; (d) form; liquid or solid to a

from the enrichment process for subsequent upon transfer from the enrichment process for subsequent upon transfer

6 6

process by compressing and converting UF including: (a) Feed autoclaves, ovens, or systems used for passing ovens, UF Feed autoclaves, systems used for or including: (a) passing ovens, UF Feed autoclaves, systems used for or including: (a) the enrichment process by compressing and converting UF UF stations used transferring for ‘Product’ or ‘tails’ (d) form; passing ovens, UF Feed autoclaves, systems used for or including: (a) the enrichment process by compressing and converting UF UF stations used transferring for ‘Product’ or ‘tails’ (d) form; the enrichment process; (b) Desublimers (or cold traps) used to remove UF (or cold traps) Desublimers the enrichment process; (b) the enrichment process; (b) Desublimers, cold traps or pumps used to remove UF designed Especially or prepared process systems equipment for enrichment by UF corrosion to resistant by materials protected or of made plants the enrichment process; (b) Desublimers, cold traps or pumps used to remove UF ‘Product’ or ‘tails’ stations used for transferring UF stations used for transferring or ‘tails’ ‘Product’ designed Especially or prepared process systems equipment for enrichment by UF corrosion to resistant by materials protected or of made plants heating; (c) Solidification or liquefaction stations used to Solidification remove UF heating; (c) or liquefaction stations used to Solidification remove UF heating; (c) Especially designed Especially or prepared process systems equipment for enrichment by UF corrosion to resistant by materials protected or of made plants from the enrichment process for subsequent upon Solidifi transfer heating; (c) cation or liquefaction stations used to remove UF TLB5.4.1 Feed systems/product and tails withdrawal systems withdrawal tails and systems/product TLB5.4.1 Feed TLB5.2.1 Feed systems/product and tails withdrawal systems withdrawal tails and systems/product TLB5.2.1 Feed TLB5.7.11 Feed systems/product and tails withdrawal systems (molecular based methods) based (molecular systems withdrawal tails and systems/product TLB5.7.11 Feed to a

from the

liquid or solid form; enrichment process by compressing, cooling and converting UF 0B002.d Liquefaction or solidification stations used to remove UF remove to used stations solidification or 0B002.d Liquefaction

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 53

, , 6 6

6 6

to to

6 6

from the enrichment from the enrichment

into containers. into containers. 6 6

-resistant materials (see

6 6

to a liquid or solid form; (d) form; liquid or solid to a (d) form; liquid or solid to a

6 6

within the centrifuge cascades. The piping within the centrifuge network is

normally of the ‘triple’ header system with each centrifuge connected system to header with each centrifuge normally of the ‘triple’ each of the headers. There is thus a substantial amount in its of repetition is wholly form. It made of or protected by UF process by compressing and converting UF process by compressing and converting UF including: (a) Feed autoclaves, ovens, or systems used for passing ovens, UF Feed autoclaves, systems used for or including: (a) passing ovens, UF Feed autoclaves, systems used for or including: (a) the enrichment process; (b) Desublimers (or cold traps) used to remove UF (or cold traps) Desublimers the enrichment process; (b) used to remove UF (or cold traps) Desublimers the enrichment process; (b) Especially designed or prepared piping Especially systems and systems for header handling UF ‘Product’ or ‘tails’ stations used for transferring UF stations used for transferring or ‘tails’ ‘Product’ UF stations used for transferring or ‘tails’ ‘Product’ Especially designed Especially or prepared process systems equipment for enrichment by UF corrosion to resistant by materials protected or of made plants to very high and EXPLANATORY is fabricated section) NOTE to this standards. vacuum and cleanliness Especially designed Especially or prepared process systems equipment for enrichment by UF corrosion to resistant by materials protected or of made plants from the enrichment process for subsequent upon Solidifi transfer heating; (c) cation or liquefaction stations used to remove UF from the enrichment process for subsequent upon Solidifi transfer heating; (c) cation or liquefaction stations used to remove UF TLB5.2.2 Machine header piping systems piping header TLB5.2.2 Machine TLB5.5.7 Feed systems/product and tails withdrawal systems withdrawal tails and systems/product TLB5.5.7 Feed TLB5.7.11 Feed systems/product and tails withdrawal systems (molecular based methods) based (molecular systems withdrawal tails and systems/product TLB5.7.11 Feed within gaseous diffusion, centrifuge or aerodynamic cascades; within gaseous diffusion, centrifuge

handling UF 0B002.e Piping systems and header systems specially designed or prepared for prepared or designed specially systems header and systems 0B002.e Piping

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 54

- 6

-bearing 6

within the

-bearing atmos 6

per minute or more.

3 , for handling UF , for 6

within the gaseous cascades. within the diffusion

vacuum pumps having a suction capacity of 5 m 5 of capacity suction vacuum pumps having a (see EXPLANATORY NOTE to this section). These pumps may be either and may seals, and fluorocarbon displacement may have positive, or rotary present. working fluids have special . These pumps may use fluorocarbon seals and special working fluids. pheres made of, or protected by, materials resistant to corrosion by UF resistant by, pheres made of, or protected materials 6

aerodynamic cascades. This piping aerodynamic cascades. network is normally of the ‘double’ header design with each stage or group of stages connected to each of the headers. Vacuum pumps especially designed or prepared for service in UF service for prepared designed Vacuum pumps or especially (a) and vacuum headers vacuum manifolds, prepared designed or Especially Especially designed or prepared piping Especially systems and systems for header handling UF to corrosion by atmospheres and resistant made of or protected by materials UF UF in service and vacuum pumps, and designed for vacuum headers folds, bearing atmospheres Especially designed header piping Especially or prepared systems, made of or protected by UF corrosion to resistant by materials EXPLANATORY NOTE This piping network is normally of the “double” the of normally is network piping This EXPLANATORY NOTE header system with each cell connected to each of the headers. TLB5.4.2 Header piping systems piping TLB5.4.2 Header TLB5.5.8 Header piping systems piping TLB5.5.8 Header TLB5.4.3a Vacuum systems TLB5.4.3a Vacuum TLB5.5.9a vacuum mani consisting of vacuum systems prepared designed or Especially TLB5.4.3b (b) Vacuum pumps especially designed for service in UF in service for designed especially pumps Vacuum TLB5.4.3b (b) TLB5.5.9b Vacuum systems and pumps and systems TLB5.5.9b Vacuum or ”; 6

bearing atmospheres

-bearing atmospheres; -bearing 6

/minute or more;

3 vacuum pumps, and designed for service in UF in service designed for pumps, and vacuum made of, or protected by, “materials resistant to corrosion by UF resistant made of, or protected by, “materials capacity of 5 m 5 of capacity 3. and consisting of vacuum manifolds, headers Vacuum systems 2. Vacuum pumps specially designed for use in UF in use for designed specially pumps 2. Vacuum 1. Vacuum manifolds, vacuum headers or vacuum pumps having a suction a having pumps vacuum or headers vacuum manifolds, 1. Vacuum 0B002.f Vacuum systems and pumps as follows: as pumps and systems 0B002.f Vacuum

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 55

gas streams and of the following: having gas streams all and of the following: having gas streams all and of the following: having gas streams all

6 6 6

mass spectrometers/ion sources mass spectrometers/ion sources mass spectrometers/ion sources mass spectrometers/Ion

6 6 6

a resolution of better than 1 part in 320; of better a resolution by alloys; % or more weight, or nickel-chrome a nickel content of 60 than 1 part in 320; of better a resolution by alloys; % or more weight, or nickel-chrome a nickel content of 60 than 1 part in 320; of better a resolution by alloys; % or more weight, or nickel-chrome a nickel content of 60 1. and Capable ions having of measuring of 320 mass units or greater atomic with alloys nickel-copper nickel, by protected or of constructed sources 2. Ion sources; ionization bombardment 3. Electron analysis. isotopic for suitable system collector a 4. Having 1. and Capable ions having of measuring of 320 mass units or greater atomic with alloys nickel-copper nickel, by protected or of constructed sources 2. Ion sources; ionization bombardment 3. Electron analysis. isotopic for suitable system collector a 4. Having 1. and Capable ions having of measuring of 320 mass units or greater atomic with alloys nickel-copper nickel, by protected or of constructed sources 2. Ion sources; ionization bombardment 3. Electron analysis. isotopic for suitable system collector a 4. Having Especially designed or prepared mass spectrometers capable of taking on-line capable spectrometers mass designed prepared or Especially UF samples from of taking on-line capable spectrometers mass designed prepared or Especially UF samples from of taking on-line capable spectrometers mass designed prepared or Especially UF samples from TLB5.2.4 UF TLB5.4.5 UF TLB5.5.11 UF and mass spectrometers/ion sources capable of taking on-line samples from mass spectrometers/ion gas streams and having all of the following: the of and having all gas streams

6 6

a resolution of better than 1 part in 320; of better a resolution alloys; by % or more weight, or nickel-chrome 60 content of with a nickel 4. Having a collector system suitable for isotopic analysis. isotopic for suitable system collector a 4. Having 1. and having Capable of measuring ions of 320 units or greater mass atomic 2. Ion sources constructed of or protected by nickel, nickel-copper alloys sources; ionisation bombardment 3. Electron UF 0B002.g UF

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 56

6 4 2

can

to UF to UF to UO

3 2

can be performed can be performed can be performed

2 2

can be performed by can be performed

to UO to UO

to UF 3 3

either by concentration and denitration or by

with cracked ammonia gas or hydrogen. with cracked ammonia gas or hydrogen. with cracked

3 3

with hydrogen fluoride gas (HF) at 300-500 °C. with hydrogen at 300-500 gas (HF) fluoride

, with a diameter of 40 mm or greater, for installation in main and installation for mm or greater, of 40 , with a diameter 6

neutralization with gaseous ammonia to produce ammonium diuranate with produce ammonium diuranate to gaseous ammonia with neutralization calcining drying, and subsequent filtering, concentrates to UO concentrates through reduction of UO of through reduction UO of through reduction Especially designed or prepared bellows-sealed valves, manual or automated, valves, bellows-sealed prepared designed or Especially to corrosion by resistant or control, made by of or protected shut-off materials UF auxiliary systems of aerodynamic enrichment plants. EXPLANATORY NOTE UO of Conversion EXPLANATORY NOTE UO of Conversion EXPLANATORY NOTE UO Conversion of EXPLANATORY NOTE be performed by first dissolving the ore in nitric acid and extracting purified acid and extracting dissolving the ore in nitric by first be performed uranyl phosphate.Next, the tributyl solvent such as using a nitrate uranyl nitrate is converted to UO reacting UO TLB7.1 designed systems for the conversion Especially or prepared of uranium ore TLB5.7.10 Special shut-off and control valves control and shut-off TLB5.7.10 Special ; TLB7.1.1 EXPLANATORY NOTE Conversion to UO of uranium ore concentrates 3

; TLB7.1.3 the conversion of UO designed systems for or prepared Especially ; TLB7.1.2 designed systems for the conversion Especially or prepared of UO ; TLB7.1.4 designed systems for the conversion Especially or prepared of UO 2

6 4

to UF to UO to UF

3 3 2

prepared therefor, as follows: prepared therefor, 0B003 Plant for the conversion of uranium and equipment specially designed or designed specially equipment and uranium of conversion the for 0B003 Plant 0B003.a Systems for the conversion of uranium ore concentrates to UO to concentrates ore uranium of conversion the for 0B003.a Systems 0B003.c Systems for the conversion of UO of conversion the for 0B003.c Systems 0B003.b Systems for the conversion of UO of conversion the for 0B003.b Systems 0B003.d Systems for the conversion of UO of conversion the for 0B003.d Systems

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 57

, 4 6 2

using

to UF to UF 2

to UO

to U metal

is performed by is performed by is performed is condensed from

conversion is often conversion is 6 4

can be performed by can be performed

is reacted at approxi is reacted

can be performed by one performed can be

to UF to UF

to UO to U metal is performed by is performed to U metal 4 6

to UCl

to UO

is hydrolyzed by solution in water, is reacted with carbon tetrachloride

. UF

. 4

is reduced and hydrolyzed to UO

are combined in ammonium water, precipitating uranyl with hydrogen at 820 °C. process, gaseous UF In the third with hydrogen 820 at

) at approximately 400 °C. In the second, UO ) at approximately 400

4 , and NH 4

carbonate. The ammonium is combined uranyl carbonate with steam and UO yield to °C 500-600 hydrogen at ammonia is added to precipitate ammonium and added diuranate, ammonia is is the diuranate to precipitate reduced to UO °C in the presence of carbon black (CAS 1333-86-4), carbon mately 700 UCl yield to chlorine monoxide, and the hot effluent gases by passing the effluent stream through a cold trap cooled trap cold through a stream effluent by passing the gases hot effluent the fluorine gas a source of °C. The process requires to –10 UF of three processes. In the first, CO plant. fabrication fuel a of stage first the as performed reduction with magnesium (large batches) or calcium (small batches). The (small reduction with batches) or calcium magnesium (large reaction is carried out at temperatures above the melting point of uranium (1 130 °C). UO of Conversion EXPLANATORY NOTE (CCl hydrogen and steam. In the second, UF second, the In steam. hydrogen and UCl EXPLANATORY NOTE Conversion of UF of Conversion EXPLANATORY NOTE UF Conversion of EXPLANATORY NOTE UF of Conversion EXPLANATORY NOTE UF of Conversion EXPLANATORY NOTE exothermic reaction with fluorine in a tower reactor. UF reduction with hydrogen. UO first, the In two processes. one of Especially designed or prepared systems for the conversion of UF of conversion the for systems prepared or designed Especially Especially designed or prepared systems for the conversion of UO of conversion the for systems prepared or designed Especially . TLB7.1.9 4

; TLB7.1.7 designed systems for the conversion Especially or prepared of UF ; TLB7.1.5 Especially designed or prepared systems for the conversion of UF of conversion the for systems prepared or designed Especially ; TLB7.1.5 ; TLB7.1.8 2

6 4

to UCl to UF to uranium metal; to UO TLB7.1.6 UF of conversion the for systems prepared or designed Especially to UF

4 4 6 6

0B003.i Systems for the conversion of UO of conversion the for 0B003.i Systems 0B003.f Systems for the conversion of UF of conversion the for 0B003.f Systems 0B003.e Systems for the conversion of UF of conversion the for 0B003.e Systems 0B003.g Systems for the conversion of UF of conversion the for 0B003.g Systems 0B003.h Systems for the conversion of UF of conversion the for 0B003.h Systems

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 58

S service. 2

S) especially designed S) especially or prepared for heavy water production 2

utilizing the water-hydrogen sulphide exchange process. These blowers or blowers sulphide exchange These process. water-hydrogen the utilizing m compressors have a throughput than or equal capacity greater to 56 second (120 000 SCFM) while operating at pressures greater than or equal or than greater pressures at 000 operating SCFM) while second (120 to 1,8 MPa (260 psi) suction and have seals designed wet H for Single stage, low head (i.e., 0,2 blowers or MPa or 30 psi) centrifugal hydrogen-sulphide compressors for (i.e., gas containing gas more circulation % H than 70 deuterium compounds and equipment especially designed or prepared therefor: (114,3 ft) m 35 to equal or than greater Ammonia-hydrogen exchange towers operating of capable m (8,2 ft) to 2,5 m (4,9 ft) 1,5 of height with diameters in 225 psi) especially designed or prepared than 15 at pressures greater MPa (2 for heavy water production utilizing the ammonia-hydrogen exchange process. opening one flanged, axial of the same least also have at These towers diameter as the cylindrical part through which the tower internals can be inserted or withdrawn. diameters of 1,5 m or greater and greater capable of operating at pressures m or greater of 1,5 diameters than or equal to 2 MPa heavy (300 designed psi), especially or prepared for water production utilizing the water-hydrogen sulphide exchange process. TLB6 and deuterium heavy water, of concentration production or the for Plants TLB6.2 Blowers and Compressors and TLB6.2 Blowers TLB6.3 Ammonia-Hydrogen Exchange Towers Exchange TLB6.3 Ammonia-Hydrogen TLB6.1 with Exchange towers — Hydrogen Sulphide Exchange Towers Water /second

S service; S service; 2

S) with a throughput capacity greater than or equal to 56 m than S) with a throughput or equal to 56 greater capacity 2

when operating at pressures greater than or equal to 1,8 MPa suction and 1,8 MPa to equal than or greater pressures at when operating H wet designed for having seals for hydrogen sulphide % gas circulation (i.e. gas containing more than 70 H height with diameters of 1,5 m to 2,5 m capable of operating at m capable of m to 2,5 1,5 of height with diameters than 15 pressures greater MPa; more, capable of operating at pressures greater than or equal greater to 2 more, capable of operating at pressures MPa; 2. Single stage, low head (i.e. 0,2 MPa) centrifugal blowers or compressors or blowers centrifugal MPa) 0,2 (i.e. head low stage, 2. Single deuterium compounds and specially designed or prepared equipment and follows: as components therefor, m in Ammonia-hydrogen than or equal to 35 exchange 3. towers greater as follows: plants; exchange sulphide 1. Water-hydrogen plants; exchange 2. Ammonia-hydrogen 1. Water-hydrogen 1. Water-hydrogen sulphide m exchange or towers with diameters of 1,5 0B004 the production Plant for or concentration of heavy water, deuterium and 0B004.a compounds, the production or deuterium deuterium for of heavy Plant water, 0B004.b Equipment and components, as follows: as components, and 0B004.b Equipment

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 59

Infrared absorption analyzers capable of “on-line” hydrogen/deuterium ratio %. analysis where deuterium concentrations are equal than to or 90 greater especially columns therefor, upgrade systems, or Complete heavy water the upgrade designed of heavy for to reactor-grade or prepared water deuterium concentration. distil water employ usually which systems, These EXPLANATORY NOTE lation to heavy separate water from light water, are especially designed or % 99,75 typically (i.e., heavy water produce reactor-grade to prepared deuterium oxide) from heavy feedstock water of concentration. lesser Tower internals and Tower internals stage pumps designed towers especially or prepared for for heavy water production utilizing the ammonia-hydrogen exchange process. designed include especially Tower internals stage contactors which promote pumps gas/liquid contact. Stage designed include especially intimate submersible pumps of for circulation liquid ammonia within a contacting to stage internal the stage towers. into heavy gas conversion deuterium the of enriched burners for Catalytic water especially designed or prepared for heavy water production utilizing the ammoniahydrogen exchange process. Ammonia crackers with operating pressures greater than or equal to 3 MPa to equal than or greater pressures operating with Ammonia crackers production utilizing heavy water for prepared designed or especially (450 psi) the ammoniahydrogen exchange process. TLB6.6 Infrared Absorption Analyzers Absorption TLB6.6 Infrared therefor columns or systems upgrade water heavy TLB6.8 Complete TLB6.4 Tower Internals and Stage Pumps Stage and Internals TLB6.4 Tower Burners TLB6.7 Catalytic TLB6.5 Ammonia Crackers Crackers TLB6.5 Ammonia analysis where deuterium concentrations are equal to or greater than 90 %; equal than are to 90 analysis where deuterium concentrations or greater concentration; deuterium reactor-grade to heavy water upgrade of those which are submersible, for heavy those which submersible, for production the are water utilizing ammonia-hydrogen exchange process; water utilizing the ammonia-hydrogen exchange process; MPa for heavy water production utilizing the ammonia-hydrogen production heavy utilizing MPa for water exchange process; 6. Infrared absorption analysers capable of on-line hydrogen/deuterium ratio hydrogen/deuterium on-line of capable analysers absorption 6. Infrared 8. Complete heavy water upgrade systems, or columns therefor, for the 4. Tower internals, including stage contactors, and stage pumps, including pumps, stage and contactors, stage including internals, 4. Tower 7. the conversion burners for gas of enriched deuterium into heavy Catalytic 5. Ammonia crackers with operating pressures greater than or equal to 3 with operating pressures greater 5. Ammonia crackers

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 60

Ammonia synthesis converters or synthesis units especially designed or especially or synthesis units Ammonia synthesis converters the ammonia-hydrogen production heavy utilizing water for prepared exchange process. EXPLANATORY NOTE or units take synthesis gas These converters (nitrogen and hydrogen) from an ammonia/hydrogen high-pressure exchange the to returned is synthesized ammonia columns), and the column (or columns). exchange column (or Plants for the fabrication of nuclear reactor fuel elements, and of nuclear Plants for the equipment reactor fabrication especially designed or prepared therefor one from manufactured are elements fuel Nuclear INTRODUCTORY NOTE mentioned in materials or more of the source or special fissionable MATERIAL AND EQUIPMENT of this annex. the most For oxide fuels, grinding and sintering, pellets, pressing equipment for fuel, of common type glove boxes (or handled in are oxide fuels Mixed be present. will grading in the cladding. cases, the sealed they until In all are equivalent containment) sealed inside a cladding suitable fuel is hermetically which is designed to be envelope encasing the primary the fuel so as to provide performance suitable of control precise cases, all operation. Also, in during reactor and safety processes, procedures and equipment high to extremely standards is fuel performance. and safe to ensure predictable in order necessary within fall to considered are that equipment of Items EXPLANATORY NOTE the meaning of the phrase “and designed equipment for especially or prepared” normally comes of fuel elements include equipment which: (a) the fabrication contact with, processes, or or directly in direct controls, the production flow of within the (b) seals the cladding; nuclear material checks (c) nuclear material; of the cladding of the (d) checks the integrity or the seal; the finish treatment Such is used fuel elements. or (e) for assembling sealed fuel; reactor equipment or systems of equipment example: 1) fully may include, for TLB6.9 Ammonia synthesis converters or synthesis units synthesis or converters synthesis TLB6.9 Ammonia

the production flow of nuclear materials; prepared for heavy production water utilizing the ammonia-hydrogen exchange process Technical Note: Specially designed or prepared equipment for the fabrication of “nuclear includes equipment reactor” fuel elements which: 1. processes or controls contact with Normally comes or directly into direct 2. Seals the nuclear within the cladding; materials 3. Checks the integrity of the cladding or the seal; 4. Checks the finish treatment of the sealed fuel; and specially designed or prepared equipment therefor. prepared designed or and specially 9. Ammonia synthesis converters or synthesis units specially designed or elements. reactor assembling for used 5. Is 0B005 Plant specially designed for the fabrication of “nuclear reactor” fuel elements elements fuel reactor” “nuclear of fabrication the for designed specially 0B005 Plant

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 61

automatic pellet inspection stations automatic pellet inspection especially stations designed or prepared for 2) pellets; fuel the of defects dimensions and surface checking final automatic welding machines especially designed or prepared for welding and inspection test automatic 3) rods); pins (or fuel onto the end caps stations especially designed or prepared for checking the of integrity designed completed fuel pins rods); 4) systems especially or prepared to (or a) includes equipment 3 typically cladding. for: Item fuel nuclear manufacture x-ray examination of pin (or rod) end cap welds, b) helium leak detection from to rods) scanning the pins (or of gamma-ray rods), and c) pins (or pressurized inside. pellets loading the fuel of correct check for especially designed or prepared therefor INTRODUCTORY NOTE plutonium and uranium from separates fuel nuclear Reprocessing irradiated fission products intensely radioactive and elements. other transuranic Different technical processes can accomplish this separation. However, over Purex has become the years the most commonly used process. and accepted acid, followed in nitric fuel nuclear Purex involves the dissolution of irradiated products by solvent uranium, plutonium, and fission the of by separation phosphateorganic diluent. Purex of tributyl in an using a mixture extraction facilities have process functions similar to each other, including: irradiated fuel element chopping, fuel dissolution, solvent extraction, and process liquor storage. There may also be equipment of for thermal denitration uranium conversion of to oxide of plutonium and treatment or metal, nitrate, nitrate fission product waste liquor to for long a form suitable term storage or the equipment of type and configuration specific disposal. However, the several for facilities Purex between may differ functions these performing to be repro fuel nuclear reasons, including the type and quantity of irradiated safety and the materials, recovered the of disposition intended and the cessed and philosophy maintenance A incorporated into the design of the facility. TLB3 Plants for the reprocessing of irradiated fuel elements, and equipment and elements, fuel irradiated of reprocessing the for TLB3 Plants

elements including equipment and components which normally the irradiated control and contact with directly direct come into fuel and the major nuclear material and fission product processing streams; a. Plant for the reprocessing of irradiated “nuclear reactor” fuel Plant for a. specially designed or prepared equipment and components therefor. Note: 0B006 includes: Note: 0B006 0B006 Plant for the reprocessing of irradiated “nuclear reactor” fuel elements, and elements, fuel reactor” “nuclear irradiated of reprocessing the for 0B006 Plant

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 62

Critically safe tanks (e.g. small diameter, annular or slab tanks) especially above, identified as plant reprocessing a use in for prepared designed or of and capable which fuel are nuclear dissolution of irradiated intended for loaded be remotely liquid, and which can highly withstanding hot, corrosive and maintained. chopped-up spent the receive normally Dissolvers EXPLANATORY NOTE is dissolved nuclear material vessels, the safe irradiated fuel. In these critically and stream. remaining hulls removed from the process acid the in nitric “plant for the reprocessing of irradiated fuel elements”, includes the equipment elements”, fuel irradiated of reprocessing the for “plant with and directly contact direct come in and components which normally and fission product nuclear material fuel and the major the irradiated control including These processes, systems for complete the processing streams. by identified production, be may plutonium conversion and metal (e.g. by taken geometry), radiation exposure the measures to avoid criticality (e.g. by (e.g. by shielding), and toxicity hazards containment). Remotely operated equipment especially designed or prepared for use in a use in for designed prepared or equipment especially Remotely operated above and plant as identified reprocessing intended to cut, chop or shear rods. bundles or assemblies, fuel nuclear irradiated EXPLANATORY NOTE This equipment breaches the cladding of the fuel to designed metal dissolution. Especially to material nuclear irradiated expose the the most commonly cutting shears are employed, although advanced may be used. lasers, equipment, such as TLB3.2 Dissolvers TLB3.1 Irradiated fuel element chopping machines chopping element fuel TLB3.1 Irradiated

operated equipment to cut, chop or shear irradiated “nuclear operated equipment to reactor” fuel assemblies, bundles or rods; or slab tanks) specially designed or prepared for the specially tanks) or slab fuel, which are dissolution of irradiated “nuclear reactor” and liquids, corrosive highly withstanding hot, capable of loaded and maintained; remotely be which can b. Fuel element chopping or shredding machines, i.e. remotely i.e. machines, shredding chopping or element b. Fuel c. Dissolvers, critically safe tanks (e.g. small diameter, annular diameter, small (e.g. tanks safe critically c. Dissolvers,

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 63

or Especially designed or prepared holding or storage vessels for use in a plant for designed holding vessels or prepared or storage Especially fuel. The for the reprocessing holding of irradiated or storage vessels must be resistant to the corrosive effect of nitric acid. The holding or storage vessels such steels, as low carbon stainless of materials normally fabricated are Holding or zirconium, or other high titanium or storage quality materials. vessels may be designed operation and for remote maintenance and may cent, per two least criticality: nuclear control of for features following have the at of equivalent boron a with structures internal or (1) walls or vessels, cylindrical for in) (7 mm 175 of diameter maximum (2) a a slab mm or annular vessel. (3 in) for either (3) a maximum width of 75 Especially designed or prepared solvent extractors such packed as or pulse designed solvent extractors or prepared Especially the for plant a in use for contactors centrifugal or settlers columns, mixer to the resistant be must extractors Solvent fuel. irradiated of reprocessing acid. of to nitric are normally Solvent fabricated corrosive effect extractors high welding standards (including special and extremely inspection and quality assurance and quality control techniques) out of low carbon stainless steels, titanium, zirconium, or other high quality materials. of solution the receive both extractors Solvent EXPLANATORY NOTE solution which separates organic and the dissolvers the from fuel irradiated the uranium, plutonium, and fission products. equipment Solvent is extraction such as operating long parameters, normally designed operating strict to meet lifetimes with no maintenance requirements or adaptability to easy variations for and flexibility and control, operation of simplicity replacement, conditions. in process TLB3.4 Chemical holding or storage vessels storage or holding TLB3.4 Chemical TLB3.3 Solvent extractors and solvent extraction equipment extraction solvent and extractors TLB3.3 Solvent

or vessel. culated for all constituent elements as defined culated for all in the note to 0C004) two of at least per cent; 1. Walls or internal structures with a boron equivalent (cal equivalent boron a with structures internal or 1. Walls 3. A maximum width of 75 mm for either a slab or annular or slab a either for mm 75 of width maximum 3. A 2. A maximum diameter of 175 mm for cylindrical vessels; cylindrical for mm 175 of diameter maximum 2. A safe and resistant to the corrosive effects of nitric acid; of nitric safe and to the corrosive effects resistant settlers or centrifugal contractors, resistant to the corrosive effects of nitric acid and specially designed or prepared for reprocessing of irradiated “natural a plant for the use in uranium”, “depleted uranium”materials”; or “special fissile Technical Note: following features: the have may Holding or storage vessels e. Holding or storage vessels specially designed to be critically be to designed specially vessels storage or e. Holding d. such Solvent extractors, as packed or pulsed columns, mixer

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 64

passed to a denitration process where it is converted to uranium oxide. to uranium converted is it where process denitration a passed to cycle. fuel in the nuclear This oxide is re-used trated by evaporation and stored as a liquor concentrate. This concentrate for suitable may be subsequently and converted to a form evaporated storage or disposal. transfer to further process steps. In particular, holding or storage vessels for plutonium solutions are designed problems resulting to avoid criticality from changes in concentration and form of this stream. nitrate to oxide EXPLANATORY NOTE Three main process liquor streams result from the from result streams liquor process main Three EXPLANATORY NOTE further used in the are vessels step. Holding storage or solvent extraction as follows: streams, three processing of all (a) The pure uranium nitrate solution is concentrated by evaporation and (b) The intensely radioactive fission products solution is normally concen Neutron measurement systems especially designed or prepared for integration designed for systems especially prepared or Neutron measurement the reprocessing plant for a systems in and use with automated process control elements. fuel of irradiated and active of capability the involve systems These EXPLANATORY NOTE the to determine in order and discrimination passive neutron measurement fissile material quantity and composition. The complete system is composed and signal processing amplifiers, a neutron a neutron detector, generator, of electronics. The scope of this entry does not include neutron detection and accountancy material nuclear designed for are that instruments measurement and use integration to not related application any other or and safeguarding of the reprocessing with automated process control systems in a plant for elements. fuel irradiated (c) The pure plutonium nitrate solution is concentrated and stored pending its pending stored and concentrated is solution nitrate plutonium pure (c) The TLB3.5 Neutron measurement systems for process control process for systems measurement TLB3.5 Neutron TLB7.2.1 designed Especially or prepared systems for the conversion of plutonium

for integration and use with automated process control systems in a plant for the reprocessing of irradiated “natural uranium”,fissile uranium”“special or “depleted materials”. f. Neutron measurement systems specially designed or prepared or designed specially systems measurement f. Neutron prepared therefor, as follows: prepared therefor, 0B007 Plant for the conversion of plutonium and equipment specially designed or designed specially equipment and plutonium of conversion the for 0B007 Plant

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 65

ss are: ion

EXPLANATORY NOTE This process usually involves the fluorination of fluorination the involves usually process This EXPLANATORY NOTE hydrogen to fluoride, with highly corrosive plutonium dioxide, normally subsequently reduced using which is high purity produce plutonium fluoride calcium metal to produce plutonium metallic and a calcium fluoride slag. The main functions involved fluorination (e.g. involving in this process are reduction (e.g. metal metal), a precious lined with or equipment fabricated handling, ventilation, product recovery, slag crucibles), employing ceramic particularly management and process control. The systems are waste toxicity and to minimize effects and radiation adapted so to avoid criticality as of plutonium processes include the fluorination oxalate or hazards. Other metal. to reduction by a plutonium peroxide followed The term “source material” means uranium containing the mixture of isotopes means uranium containing the mixture “source material” The term the isotope 235; any of the uranium depleted in thorium; in nature; occurring compound, any alloy, chemical or concentrate; metal, of form the foregoing in containing one other material or more of the foregoing in such concentration as the Board of Governors shall from time to time determine; and such other determine. time to as the Board of Governors shall from material process feed storage and solid/liquor separation, process feed adjustment, precipitation product handling, management, and process ventilation, waste calcination, adapted so as control. The to avoid process systems are particularly criticality most reprocessing In hazards. toxicity and to minimize effects and radiation facilities, this process involves the conversion of plutonium nitrate to of precipitation involve the can processes plutonium dioxide. Other plutonium peroxide. or plutonium oxalate 1.1. “Source material” “Source 1.1. TLA.1.1

non-nuclear applications: uranium” when contained in a sensing component instruments; in b. “Depleted uranium” specially fabricated for the following civil b. a. Four grammes of “natural uranium”or less or “depleted a. Note: 0C001 does not control the following: the control not does Note: 0C001 alloy, chemical compound containing alloy, chemical and any or concentrate other material one foregoing; or more of the 0C001 uranium” or “depleted uranium” thorium in “Natural the form of metal, 0B007.a a. Systems for the conversion of plutonium nitrate to oxide; EXPLANATORY NOTE The main functions involved in this proce oxide; this to in nitrate involved plutonium functions of main conversion The the NOTE EXPLANATORY for Systems 0B007.a a. 0B007.b Systems for plutonium metal production. b. TLB7.2.2 Especially designed or prepared systems for plutonium metal product

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 66

233; “uranium enriched in the isotopes 235 233”;the any material in or 233; “uranium enriched containing of the foregoing; and one such or more other fissionable material as the Board of Governors shall from time to time determine; does not include source material. material” fissionable “special but the term the that amount such an both in 233 or 235 or isotopes the containing abundance of the sum of these isotopes to the isotope ratio 238 is greater than of the isotope 235 the ratio to the isotope 238 occurring in nature. kilograms. 80 %. when used or less as a quantities in gram material fissionable Special 000 and sensing component instruments; in which is to be used the Government is satisfied only Source material in such as the production of alloys or ceramics; non-nuclear activities, Natural uranium Depleted uranium Thorium 1 500 kilograms; 000 kilograms; and 1 i) The term “special fissionable material” means plutonium-239; uranium- plutonium-239; means material” fissionable “special term i) The uranium means 233” or 235 isotopes the in enriched “uranium term ii) The However, for the purposes in subparagraph of the Guidelines, items specified below, to (a) and a given material exports of source or special fissionable recipient country, within a period of 12 months, below the limits specified in not be included: below, shall subparagraph (b) (a) Plutonium with an isotopic concentration of plutonium-238 exceeding (b) Special fissionable material 50 effective grams; 1.2. “Special fissionable material” fissionable “Special 1.2. TLA.1.2

1. Shielding; 2. Packaging; kg; 100 than greater not mass a having 3. Ballasts kg; 100 than greater not mass a having 4. Counter-weights factured for non-nuclear use. c. Alloys containing less than 5 % thorium; % 5 than less containing c. Alloys manu Ceramic products containing have been thorium, which d. contained in a sensing component in instruments. Note: 0C002 does not control four “effective grammes” or less when 0C002 “Special fissile materials” fissile 0C002 “Special

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 67 ); are the atomic masses z

× A

B and A σ

since carbon is not considered

for use in a as nuclear reactor

3 carbon

) divided by (

× A

Z σ for impurities (excluding BE

are the thermal neutron capture cross sections (in barns) for naturally

σ (ppm) = CF × concentration of element Z (in ppm);

and Z

B Deuterium, heavy water (deuterium oxide) and any other deuterium compound deuterium oxide) and any other (deuterium heavy water Deuterium, 000 use for in in which of deuterium to hydrogen the ratio atoms exceeds 1:5 as defined in paragraph 1.1. reactor a nuclear above in quantities exceeding kg any country of deuterium atoms for in one recipient any period of 12 200 months. defined in paragraph 1.1 defined above, exceeding 1 kilogram. in quantities EXPLANATORY NOTE whether or the purpose determine For of export control, the Government will nuclear for are the above graphite meeting specifications not the exports of use. reactor as the calculated or is xperimentally Boron may be determined equivalent (BE) BE sum of ( conversion factor: the CF is σ an impurity) including boron, an impurity) where: BE Graphite having a purity than level better 5 parts per million boron equivalent g/cm than 1,50 density greater and with a of naturally occurring boron and element Z respectively. occurring boron and element Z respectively; and A and respectively; Z boron and element occurring 2.2. Nuclear grade graphite grade Nuclear 2.2. 2.1. Deuterium and heavy water heavy and Deuterium 2.1. TLB2.2 TLB2.1 for

are the

Z and A

B for use in a “nuclear

Z A A

Z B

σ σ since carbon not is considered an

= carbon

are the thermal neutron capture cross sections (in barns) for are the thermal neutron (in capture cross sections

σ Member State in which the exporter is established will determine will established in which the exporter is Member State above specifi whether or not the exports of graphite meeting cations are for “nuclear reactor” use. impurities (excluding BE impurity) including boron, where: and

B (ppm) = CF × concentration Z in ppm; of element σ

where CF is the conversion factor the where CF is Note 1: For the purpose of export control, the competent authorities reactor”, in quantities exceeding 1 kg. exceeding 1 in quantities reactor”, 1C107 ALSO N.B.: SEE Note 2: In 0C004, ‘boron equivalent’ (BE) is defined as the sum of BE of sum the as defined is (BE) Note 2: equivalent’ ‘boron 0C004, In deuterium, and mixtures and solutions containing deuterium, in which the 000. isotopic ratio of deuterium to hydrogen exceeds 1:5 alent’ and with a density greater than 1,50 g/cm and alent’ with a than density 1,50 greater BE atomic masses of naturally occurring boron and Z respectively. element and naturally occurring boron and element Z respectively; and A respectively; Z boron and element occurring naturally 0C004 Graphite having a purity level better than 5 parts per million ‘boron equiv ‘boron million per parts 5 than better level purity a having 0C004 Graphite 0C003 Deuterium, heavy water (deuterium oxide) and other compounds of compounds other and oxide) (deuterium water heavy 0C003 Deuterium,

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 68

-resistant fully fluorinated hydrocarbon 6

refer to items listed in refer Annex A of NSG Part 1 Trigger List. Item codes marked m, and a high degree of particle size uniformity, which are especially which are uniformity, size of particle high m, and a degree filters. μ polymers having a purity of 99,9 % by weight or more, a particle size less than % by weight or more, polymers having a particle a purity of 99,9 10 barriers. gaseous diffusion of manufacture the for prepared (b) especially prepared compounds or powders for the manufacture of such of manufacture the for powders compounds or prepared (b) especially % or Such compounds and powders alloys containing 60 include nickel or more nickel, aluminium oxide, or UF may duction”,contained This information or “use” of any in the List. item take the form of “technical data”, or “technical assistance”. fixed in any tangible medium may take of expression. assistance” “technical forms such as: instruction, skills, training, working knowledge, consulting services.

TLB* “technology” means specific information required for the “development”, “pro “development”, the for required information specific means TLB* “technology” TLB* means of one a collection or “microprograms” or “software” more “programs” TLB5.3.1b Gaseous diffusion barriers and barrier materials barrier and barriers diffusion TLB5.3.1b Gaseous (e.g. nickel or alloy

m measured by American Society for Society by American m measured μ containing 60 or more nickel, aluminium oxide weight per cent and fully % by weight or hydrocarbon having polymers), fluorinated a purity of 99,9 than size less 10 more and a particle (ASTM) B330 Testing and Materials standard and a high degree of particle size uniformity. opment”, “production”of goods or “use” in this Category. specified II* IV diffusion barriers, resistant to corrosion by UF resistant diffusion barriers, duction” of goods or “use” in this Category. specified II* IV* 0E001 T* “Technology” according to the Nuclear Technology Note for the “devel 0C005 Specially prepared compounds or powders for the manufacture of gaseous of manufacture the for powders or compounds prepared 0C005 Specially OD001 T*“Software” specially designed or modified for the “development”, “pro “development”, the for modified or designed specially OD001 T*“Software” with neither “TLB” nor “TLA” refer to items listed in the NSG to items Dual in the Categories with neither “TLB”Use 1, nor List, referenced refer 2 and “TLA” 6. ) codes to items listed in Annex marked Item with a “TLB” refer B codes of the NSG marked List. Item Part 1 with “TLA” Trigger

1 ( M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 69

1. Exploding bridge (EB); bridge 1. Exploding (EBW); wire bridge 2. Exploding 3. Slapper; (EFI); initiators foil 4. Exploding charged, explosively-driven and optically-driven firing sets designed to sets firing charged, explosively-driven and optically-driven 6.A.1. by Item detonators specified above; controlled drive multiple a. Electrically driven explosive detonators, as follows: as detonators, explosive driven a. Electrically a. Detonator firing sets (initiation systems, firesets), including electronically- including firesets), systems, (initiation sets firing a. Detonator Nuclear Suppliers Group's as in control list INFCIRC/254/Rev.9/Part2 6.A.1. Detonators and multipoint initiation systems, as follows: as systems, initiation multipoint and 6.A.1. Detonators 6.A.2. as follows: pulse generators, and equivalent high-current sets Firing

CATEGORY 1 — SPECIAL MATERIALS AND RELATED EQUIPMENT MATERIALSAND SPECIAL — CATEGORY 1

transit of dual-use items detonator. electrical conductor (bridge, bridge wire, or foil) that explosively passed pulse is vaporises when through a fast, high-current electrical it. In non-slapper types, the exploding conductor starts a chemical (pen such as PETN material contacting high explosive detonation in a In taerythritoltetranitrate). or slapper a across flyer drives a gap, and the impact of slapper on some designs is detonation. slapper in a chemical The starts an explosive driven by magnetic force. The term exploding detonator foil may to refer either an EB or a slapper-type detonator. 1. Exploding bridge (EB); bridge 1. Exploding (EBW); wire bridge 2. Exploding 3. Slapper; (EFI). initiators foil 4. Exploding Technical Notes: The word 1. initiator or igniter is sometimes used in place of the word 2. For the purpose of 1A007.b. the detonators a of concern small all utilise 3. slapper detonators, conductor vaporization the explosive of the electrical containing “energetic materials”, by electrical means, as follows: as means, by electrical materials”, containing “energetic 1A007 Equipment and devices, specially designed to initiate charges and devices and charges initiate to designed specially devices, and 1A007 Equipment 1A007 b. Electrically driven explosive detonators as follows: as detonators explosive driven Electrically 1A007 b. 2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and brokering exports, transfer, of control the for 5 Community 2009 of regime a up May 2009 setting The corresponding Council No 428/ in systems, equipment Regulation (EC) and components identified as Components and Equipment 1A Systems, M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 70

;

2 ; and

3 2.C.7.a. or carbon prepreg materials specified in Item 2.C.7.c. Item in specified materials prepreg carbon 2.C.7.a. or and b. A density greater than 3 g/cm 3 than greater density b. A acteristics: acteristics: and mm; 400 and 75 between of diameter inside a. An b. specified in Item Made with any materials” of the “fibrous or filamentary ordinary water, having ordinary water, both of the following characteristics: wettability; improve to treated chemically mesh bronze phosphor of a. Made b. Designed towers. to be used in vacuum distillation c. A thickness of 100 mm or greater. or mm 100 of thickness c. A the following characteristics, and specially designed frames therefor: designed and specially frames the following characteristics, m a. than 0,09 greater area’ A ‘cold Technical Note: 1.A.1.a. Item In ‘cold area’means the term the viewing area of the window of radiation exposed level in the design to the lowest application. isotope exchange between hydrogen reaction the recovery of for and water production from heavy or for the of heavy water tritium water. 2.A.3. of tubes having both in the form of the following char Composite structures 4.A.1. Specialized packings which may be used in separating heavy water from water heavy separating in used be may which packings 4.A.1. Specialized 1.A.1. High-density (lead glass or other) radiation shielding windows, having all of all having windows, shielding radiation other) or glass (lead 1.A.1. High-density 2.A.2. Platinized catalysts specially designed or prepared for promoting the hydrogen the promoting for prepared or designed specially catalysts 2.A.2. Platinized

and

;

2 and ;

3 1C010.a. or b. or 1C210.a. specified or materials with carbon prepreg in 1C210.c. and specified in 1A007.b.; b. A density greater than 3 g/cm 3 than greater density b. A b. Made with any of the “fibrous or filamentary materials” specified in b. Designed towers. to be used in vacuum distillation ordinary water, having both of the following characteristics: a. Made to improve wettability; of phosphortreated bronze mesh chemically N.B.: 3A232. GOODS CONTROLS, 3A229 AND MILITARY ALSO SEE a. Explosive detonator firing sets designed to drive explosive detonators c. mm or greater. A thickness of 100 Technical Note: In 1A227 means area’the term ‘cold the viewing area of the window exposed of radiation level in the design to the lowest application. the following characteristics, and specially designed frames therefor: designed and specially frames the following characteristics, m 0,09 than greater area’ ‘cold a. A hydrogen isotope exchange reaction between hydrogen and water for the for water hydrogen and between reaction exchange hydrogen isotope from heavy of recovery water or for the production tritium of heavy water. tubes and having both characteristics: of the following 9A110. AND 9A010 ALSO N.B.: SEE mm; 400 and mm 75 between of diameter inside a. An 1A226 Specialized packings which may be used in separating heavy water from water heavy separating in used be may which packings 1A226 Specialized 1A227 High-density (lead glass or other) radiation shielding windows, having all of all having windows, shielding radiation other) or glass (lead 1A227 High-density 1A225 promoting the for designed or prepared specially catalysts Platinized 1A202 of in 1A002,form in the than those specified other Composite structures,

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 71

unit difference is inherently capable of enriching the isotopes of is inherently capable of enriching unit difference mass difference. uranium with a three-unit dinated and programmed in two or more axes; and materials”; or filamentary “fibrous greater; mm or 300 mm and lengths of 75 and 650 1. Having motions for positioning, wrapping, and winding fibers coor 2. from or laminates composite structures designed Specially to fabricate between diameter internal an with tubes cylindrical winding of 3. Capable specified in Item 3.B.4.a.; 3.B.4.a. as those for uranium. as those for and the magnetic field those configurations in external to which they are the field. 250 g of fluorine per hour. a. Filament winding machines having all of the following characteristics: following the of all having machines winding a. Filament machines winding filament the for controls programming and b. Coordinating Item in specified machines winding filament the for mandrels c. Precision multiple ion sources capable of providing a total ion beam current of 50 mA current ion beam providing total capable of a ion sources multiple or greater. Notes: 1. isotopes 3.B.5. as well capable of enriching stable Item includes separators N.B.: one-mass with a isotopes of lead the of separating capable A separator in both collectors and sources ion the with separators includes 3.B.5. 2. Item Technical Note: g of separated highly ion source cannot produce more than 3 single 50 mA A enriched uranium per year from natural (HEU) abundance feed. Nuclear Suppliers Group's as in control list INFCIRC/254/Rev.9/Part2 3.B.1. Electrolytic cells for fluorine production with an output capacity greater than greater capacity output an with production fluorine for cells 3.B.1. Electrolytic 3.B.4. Filament winding machines and related equipment, as follows: as equipment, related and machines winding 3.B.4. Filament 3.B.5. Electromagnetic isotope separators designed for, or equipped with, single or single with, equipped or for, designed separators isotope 3.B.5. Electromagnetic

and

transit of dual-use items

those configurations to the field. are in which external they a. Capable of enriching stable isotopes; stable enriching of a. Capable b. With the ion sources and both and collectors in the magnetic field dinated and programmed in two or more axes; materials”; or filamentary “fibrous 75 and 650 mm and lengths of 300 mm or greater; 1. Having motions for positioning, wrapping, and winding fibres coor winding fibres positioning, wrapping, and for motions 1. Having from laminates or structures composite fabricate to designed 2. Specially 3. Capable of winding cylindrical tubes with an internal diameter between diameter internal an with tubes cylindrical winding of 3. Capable in 1B201.a.; machines specified 1B201.a. 250 g of fluorine per hour. and related equipment, as follows: equipment, as and related characteristics: following the of all having machines winding a. Filament Note: 1B226 includes separators: includes Note: 1B226 multiple ion sources capable of providing a total ion beam current of 50 ion sources capable of providing ion mA multiple beam current a total or greater. b. Coordinating and programming controls for the filament winding c. Precision mandrels for the filament winding machines specified in 1B225 Electrolytic cells for fluorine production with an output capacity greater than greater capacity output an with production fluorine for cells 1B225 Electrolytic 1B201 Filament winding machines, other than those specified in 1B001 or 1B101, or 1B001 in specified those than other machines, winding 1B201 Filament 1B226 Electromagnetic isotope separators designed for, or equipped with, single or single with, equipped or for, designed separators isotope 1B226 Electromagnetic 2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and brokering exports, transfer, of control the for 5 Community 2009 of regime a up May 2009 setting The corresponding Council No 428/ in systems, equipment Regulation (EC) and components identified as Equipment Production and Inspection 1B Test, M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 72 -compatible; and 2

production of heavy water, see INFCIRC/254/Part 1 (as amended). (as 1 INFCIRC/254/Part see heavy water, production of austenitic ASTM (or equivalent standard) grain size number of 5 or or greater; standard) grain size number of 5 or greater; and size number standard) grain of 5 or greater; 1. Stainless steel of the 300 series with low sulfur content and with an of the 300 with low sulfur 1. series steel Stainless H and cryogenic both are which materials 2. Equivalent or greater. characteristics: characteristics: 1. of 2 MPa or greater; at pressures Can operate equivalent (or ASTM austenitic an having steel carbon of 2. Constructed greater; or m 1,8 of diameter a 3. With specified in Item 4.B.1.a. istics: a. °C) or less; of 35 K temperatures (–238 Designed operation at internal for MPa; 5 to 0,5 of pressures internal at operation for b. Designed either: of c. Constructed d. With internal diameters of 30 cm or greater and ‘effective lengths’ of 4 m lengths’ of 4 and ‘effective cm or greater d. of 30 diameters internal With Technical Note: height of packing means material in a the active length’ The term ‘effective packed-type column, or height of the active internal contactor plates in a column. plate-type follows: N.B.: For columns which following are the especially of designed all or having prepared columns, for tray the exchange sulfide a. Water-hydrogen columns tray exchange sulfide water-hydrogen the for contactors b. Internal Technical Note: which have of the columns segmented trays an are effective contactors Internal counter designed to facilitate are m or greater; of 1,8 assembled diameter a carbon with steels stainless of constructed and are contacting current % or less. These may be sieve trays, valve bubble cap content of 0,03 trays or turbogrid trays. 4.B.2. Hydrogen-cryogenic distillation columns having all of the following character following the of all having columns distillation 4.B.2. Hydrogen-cryogenic 4.B.1. Water-hydrogen sulfide exchange tray columns and internal contactors, as contactors, internal and columns tray exchange sulfide 4.B.1. Water-hydrogen and -compatible; 2

and

production 0B004. of heavy water see standard) grain size number standard) grain of 5 or greater; austenitic ASTM (or equivalent standard) grain size number of 5 grain size or ASTM equivalent standard) (or austenitic greater; following characteristics: 1. of 2 MPa or greater; at pressures Can operate equivalent (or ASTM austenitic an having steel carbon of 2. Constructed 1. with low sulphur of the 300 content and steel series with an Stainless or greater. m or greater; 3. of 1,8 a diameter With 1B229.a. in columns specified 2. Equivalent materials which are both cryogenic and H and cryogenic both are which materials 2. Equivalent a. Water-hydrogen a. Water-hydrogen sulphide exchange tray columns, having all of the follows: N.B.: For columns which are specially designed or prepared for the d. With internal diameters of 30 cm or greater and ‘effective lengths’ of 4 m d. lengths’ of 4 and ‘effective cm or greater of 30 diameters With internal Technical Note: length’ means In 1B228 the active height of ‘effective packing material in a packed-type column, height or the of internal contactor active plates in a plate-type column. acteristics: acteristics: a. of 35 K (–238 temperatures operation with internal Designed °C) or less; for MPa; 0,5 5 b. to of pressure an internal at operation Designed for either: of c. Constructed b. ‘Internal contactors’ for the water-hydrogen sulphide exchange tray Technical Note: contactors’ of the columns ‘Internal are segmented trays which have an m or greater, are designed to facilitate assembled diameter of 1,8 effective with a steels countercurrent contacting and are constructed of stainless trays, valve trays, sieve be may These less. or % 0,03 of carbon content turbogrid bubble cap trays, or trays. 1B229 Water-hydrogen sulphide exchange tray columns and ‘internal contactors’, as contactors’, ‘internal and columns tray exchange sulphide 1B229 Water-hydrogen 1B228 Hydrogen-cryogenic distillation columns having all of the following char following the of all having columns distillation 1B228 Hydrogen-cryogenic

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 73

), having all of the following 3

/NH 2

/h; and

(–250 °C) (–250 or less, with heat removal capacity greater than 150 W; as the storage medium. or purification operating pressure of 1,5 to 60 MPa; or 60 MPa; 1,5 to of pressure operating pressure of 20 to 60 MPa. handling of tritium; handling of units capable of cooling to 23 Hydrogen K or helium refrigeration 1. hydrides metal using systems purification or storage isotope 2. Hydrogen less; and 1. For concentrated potassium amide % solutions or (1 greater), an 2. For dilute potassium amide solutions %), (less an than operating 1 amide catalyst in liquid ammonia (KNH characteristics: characteristics: sealed); hermetically (i.e., a. Airtight m 8,5 than greater capacity b. A a. concentration or the production, extraction, for plants recovery, or Facilities b. or plants, as follows: facilities Equipment for tritium a. Designed for operation with an outlet temperature of 35 K (– 238 °C) or °C) following characteristics: 238 (– K 35 of temperature outlet an with operation for a. Designed kg/h or greater. b. 000 Designed for a throughput of hydrogen gas of 1 c. Either of the following characteristics: following the of c. Either 2.B.1. or plants, and as follows: equipment therefor, facilities Tritium 4.A.2. Pumps capable of circulating solutions of concentrated or dilute potassium dilute or concentrated of solutions circulating of capable 4.A.2. Pumps 4.A.3. having Turboexpanders or turboexpander-compressor sets both of the ), having all of the following 3

or /NH 2

and /h;

3 and (–250 °C) (–250 or less, with heat removal capacity greater than 150 W; medium. storage or purification as the operating pressure of 1,5 operating pressure to 60 MPa; pressure of 20 to 60 MPa. or handling of tritium; units capable of cooling to 23 Hydrogen K 1. or helium refrigeration hydrides metal using systems purification or storage isotope 2. Hydrogen 1. For concentrated potassium amide solutions (1 % or greater), an % or greater), potassium For concentrated amide solutions (1 1. less; 2. For dilute potassium amide solutions (less than 1 %), an operating than potassium amide solutions 1 For dilute (less 2. a. Facilities or plants for the production, recovery, extraction, concentration, extraction, recovery, production, the for plants or a. Facilities b. or plants, as follows: facilities tritium Equipment for characteristics: sealed); hermetically (i.e., a. Airtight m 8,5 than greater capacity b. A characteristics: following the of c. Either or °C) following characteristics: (–238 K 35 of temperature outlet an with operation for a. Designed kg/h or greater. b. 000 a throughput Designed for of hydrogen gas of 1 amide catalyst in liquid ammonia (KNH amide catalyst 1B231 or plants, and as follows: equipment therefor, facilities Tritium 1B232 Turboexpanders or turboexpander-compressor sets having both of the 1B230 solutions or dilute potassium of concentrated Pumps capable of circulating

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 74

plasma separation process (PSP) are also plasma separation process applicable to are directly uranium (PSP) under INFCIRC/254 1 (as controlled Part and are isotope separation amended). amalgams; greater; and greater; mercury amalgam process, as follows: as process, amalgam mercury lithium designed for exchange columns specially liquid-liquid 1. Packed pumps; amalgam lithium or 2. Mercury cells; electrolysis amalgam 3. Lithium solution; hydroxide lithium concentrated for 4. Evaporators specially designed component parts therefor; ethers) specially designed for lithium isotope separation, and specially therefor. designed component parts containment devices designed for the testing of high containment devices designed the testing explosives or explosive for devices and having both of the following characteristics: kg of TNT or a. Designed to fully contain an explosion equivalent to 2 therefor, as follows: therefor, the for components and equipment separation isotope lithium N.B.: Certain a. isotopes; of lithium or plants for the separation Facilities isotopes based on of lithium the lithium- the separation Equipment for b. c. Ion exchange designed systems specially for lithium isotope separation, and lariat or cryptands, ethers, crown (employing systems exchange d. Chemical 2.B.2. and systems equipment plants, or facilities separation isotope Lithium similar other and containers chambers, vessels, containment explosive 5.B.7. High amalgams; mercury amalgam process, as follows: as process, amalgam mercury lithium for designed specially columns exchange liquid-liquid 1. Packed pumps; amalgam lithium or 2. Mercury cells; electrolysis amalgam 3. Lithium solution; hydroxide lithium concentrated for 4. Evaporators designed components therefor; and specially ethers), specially designed for lithium isotope separation, and specially designed components therefor. containment devices designed of high for the testing explosives or explosive devices and having both of the following characteristics: therefor, as follows: therefor, a. isotopes; of lithium or plants for the separation Facilities b. of lithium isotopes based on the separation Equipment the lithium- for separation, isotope lithium for designed specially systems exchange c. Ion lariat or cryptands, ethers, crown (employing systems exchange d. Chemical 1B233 and equipment and systems plants, or facilities separation isotope Lithium similar other and containers chambers, vessels, containment explosive 1B234 High

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 75

diagnostic or measurement information. diagnostic or measurement (20 °C); mm with an of more than outside 75 diameter (20 °C); b. of time or delayed transfer enabling Having real or features design elements a. strength of 460 tensile of’ an MPa or more at 293 ‘Capable ultimate K b. (including forgings) solid forms cylindrical of tubes or form and b. In the Technical Note: 2.C.1. In Item of’ encompasses aluminium alloys before or the phrase ‘capable after heat treatment. a. strength of 900 tensile of’ an MPa or more at 293 ‘Capable ultimate K In the form of tubes or solid cylindrical forms (including forgings) with an mm. than 75 more of outside diameter Technical Note: 2.C.13. In Item the phrase ‘capable of’ encompasses titanium alloys before or after heat treatment Nuclear Suppliers Group's as in control list INFCIRC/254/Rev.9/Part2 2.C.1. Aluminium alloys having both of the following characteristics: characteristics: following the of both having alloys 2.C.1. Aluminium 2.C.13. Titanium alloys having both of the following characteristics:

transit of dual-use items and and and

with an outside diameter of more than 75 mm. of more than 75 with an outside diameter (20 °C); an outside diameter of more than 75 mm; than 75 of more an outside diameter (20 °C); 2. In the form of tubes or cylindrical solid forms (including forgings) solid forms of tubes or cylindrical 2. In the form greater; information. of diagnostic or measurement 1. of 900 strength MPa or more at 293 tensile K of’ an ultimate ‘Capable 2. with (including forgings) solid forms tubes or cylindrical of In the form 1. of 460 at 293 strength MPa or more K tensile ‘Capable of’ an ultimate Technical Note: The phrase alloys ‘capable encompasses of’ heat alloys before or after treatment. a. Aluminium alloys having both of the following characteristics: following the of both having alloys a. Aluminium b. Having design elements or features enabling real time or delayed transfer delayed or time real enabling features or elements design b. Having N.B.: SEE ALSO MILITARY GOODS CONTROLS. GOODS MILITARY ALSO N.B.: SEE or TNT of kg 2 to equivalent explosion an contain fully to a. Designed

1C202 in 1C002.b.3. Alloys, other than those specified or .b.4., as follows: 1C202 b. Titanium alloys having both of the following characteristics: 2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and brokering exports, transfer, of control the for 5 Community 2009 of regime a up May 2009 setting The corresponding Council No 428/ in systems, equipment Regulation (EC) and components identified as 1C Materials M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 76

divided

when measured at a at when measured

3 m or greater;

4 m or greater;

4 m or greater; or m or greater;

6 m or greater; and m or greater;

6 when measured at a temperature of 296 ± 2 K when a temperature measured at

divided by the specific weight in N/m weight in divided by specific the

2 having 0,25 % or more by weight of an ester based fiber surface modi surface based by fiber % or more weight of an ester having 0,25 fier. (23 ± 2 °C) and a relative humidity of 50 ± 5 %. ± 5 humidity °C) and of 50 a relative ± 2 (23 N/m by the specific weight in N/m in weight specific by the temperature of 296 ± 2 K ± (23 2 °C) and a relative humidity of 50 ± 5 %. “tapes” with a width of 15 mm or less (prepregs), made from carbon mm made from or less (prepregs), or with a width “tapes” of 15 2.C.7.a. in Item specified or Item materials” or filamentary glass “fibrous 2.C.7.b. 2. A “specific tensile strength” of 23,5 × 10 × 23,5 of strength” tensile “specific 2. A following characteristics: 10 × 12,7 of modulus” “specific 1. A acteristics: acteristics: 10 × 3,18 of modulus” “specific 1. A Note: Item 2.C.7.a. does not control aramid “fibrous or filamentary materials” materials” filamentary or “fibrous aramid control not does 2.C.7.a. Note: Item 2. In Item 2.C.7. “Specific tensile strength” is the ultimate tensile strength in a. Carbon or aramid “fibrous or filamentary materials” having of the either a. materials” Carbon “fibrous or filamentary or aramid 2. A “specific tensile strength” of 7,62 × 10 × 7,62 of strength” tensile “specific 2. A Technical Note: of the composite. the matrix forms The resin Technical Notes: N/m in modulus Young's the is modulus” “Specific 2.C.7. Item 1. In 2.C.7.a and prepregs, as follows: materials”, or filamentary “Fibrous 2.C.7.c c. Thermoset resin impregnated continuous “yarns”, “rovings”, “tows” or “tows” “rovings”, “yarns”, continuous impregnated resin Thermoset 2.C.7.c c. 2.C.7.b having both of the following materials” char “fibrous or filamentary Glass

and or m or greater; m or greater;

4 4

m or greater; m or greater;

6 6

having 0,25 % by % weight or more of an ester based fibre surface having 0,25 modifier; “monofilaments”, “yarns”, “rovings”, “tows” or “tapes”. “tapes” with a width of 15 mm or less (prepregs), made from carbon or mm or less (prepregs), with a width of 15 “tapes” specified in 1C210.a. glass ‘fibrous materials’ or filamentary or b. 2. A “specific tensile strength” of 7,62 × 10 × 7,62 of strength” tensile “specific 2. A acteristics: acteristics: 10 × 3,18 of modulus” “specific 1. A 2. A “specific tensile strength” of 23,5 × 10 × 23,5 of strength” tensile “specific 2. A following characteristics: 10 × 12,7 of modulus” “specific 1. A c. impregnated continuous resin “yarns”, “rovings”,Thermoset or “tows” Note: 1C210.a. does not control aramid ‘fibrous or filamentary materials’ filamentary or ‘fibrous aramid control not Note: 1C210.a. does 1C010.a., b. or e., as follows: a. of the having either materials’ or filamentary Carbon ‘fibrous or aramid b. having both materials’ of the following char or filamentary Glass ‘fibrous Technical Note: of the composite. The resin forms the matrix continuous to restricted is materials’ filamentary or ‘fibrous 1C210, Note: In 1C210 or prepregs, other than those in specified materials’ ‘Fibrous or filamentary

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 77

B) isotope to greater than its natural than its greater B) isotope to

75 mm or less. weights or gamma-ray collimators. weights or gamma-ray materials. with an inside diameter between 100 and 300 mm; and with an between 100 inside diameter and 300 at 293 K (20 °C). at 293 K (20 Note: dimensions are linear which all in 2.C.11. forms Item does not control Technical Note: In Item 2.C.11. the phrase ‘capable of’ encompasses maraging steel before or after heat treatment. weight, having both of the following characteristics: segments) cylinder (including symmetry cylindrical hollow a with forms a. In kg. 20 than greater mass b. A Note: Item 2.C.14. does not control manufactures specially designed as isotopic abundance, as follows: elemental boron, isotopic abundance, elemental compounds, as follows: mixtures of any of the fore or scrap waste containing boron, thereof, manufactures going. boron loaded containing boron include 2.C.4. mixtures Item In Note: Technical Note: isotopic abundance The natural of boron-10 approximately 18,5 is weight percent (20 atom percent). 2.C.4. Boron enriched in the boron-10 ( boron-10 the in enriched 2.C.4. Boron 2.C.11. 950 MPa or more of 1 tensile strength an ultimate of’ ‘capable Maraging steel 2.C.14. tungsten by % than 90 containing more and alloys Tungsten, tungsten carbide,

and

B) isotope to greater than its natural than its B) isotope to greater

gamma-ray collimators. 75 mm or less.

segments) with an inside diameter between 100 mm and 300 mm; Technical Note: The phrase maraging ‘capable encompasses of’ steel maraging before steel heat treatment. or after Note: boron loaded materials. containing boron include 1C225 mixtures In Technical Note: The natural isotopic abundance of boron-10 approximately 18,5 is weight (20 atom per cent). per cent kg. 20 than greater mass b. A isotopic abundance, as follows: elemental boron, isotopic abundance, elemental compounds, as follows: mixtures containing or scrap of any of the fore waste boron, thereof, manufactures going. by weight, other than that specified by 1C117, following specified the having both of than that by weight, other characteristics: a. In forms with a hollow cylindrical symmetry (including cylinder or weights as designed specially manufactures control not does Note: 1C226 tensile strength of 1 950 MPa or more, at 293 K (20 °C). 950 MPa or more, at 293 K (20 of 1 strength tensile Note: 1C216 does not control forms in which all linear dimensions are 1C226 Tungsten, tungsten carbide, and alloys containing more than 90 % tungsten % 90 than more containing alloys and carbide, tungsten 1C226 Tungsten, 1C216 Maraging steel, other than that specified in 1C116, ‘capable of’ an ultimate an of’ ‘capable 1C116, in specified that than other steel, 1C216 Maraging ( boron-10 the in enriched 1C225 Boron

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 78

designed for electronic component parts or as substrates for elec for substrates as or component parts electronic designed for tronic circuits; or aquamarines. a. Metal windows for X-ray machines or for bore-hole logging devices; logging bore-hole for or machines X-ray for windows a. Metal b. Oxide shapes in fabricated or semi-fabricated forms specially c. of emeralds the form in and aluminium) of beryllium Beryl (silicate other than calcium; and other than calcium; impurities other than magnesium; and beryllium compounds, manufactures thereof, and waste or scrap of any of of scrap or and waste compounds, thereof, beryllium manufactures the foregoing. following: the control not does 2.C.2. Note: Item a. Containing less than 200 parts per million by weight of metallic impurities metallic of weight by million per parts 200 than less a. Containing b. boron. by weight of million per Containing than 10 parts less a. Containing 000 less than parts 1 per million by weight of metallic b. boron. by weight of million per Containing than 10 parts less a. by weight; and % or greater A purity of 99,99 silver. of weight by million) per (parts ppm 10 than less b. Containing 2.C.2. Beryllium metal, alloys containing more than 50 % beryllium by weight, by beryllium % 50 than more containing alloys metal, 2.C.2. Beryllium 2.C.3. Bismuth having both of the following characteristics: following the of both having 2.C.3. Bismuth 2.C.5. Calcium having both of the following characteristics: characteristics: following the of both having 2.C.5. Calcium 2.C.10. Magnesium having both of the following characteristics: following the of both having 2.C.10. Magnesium

and and

and devices; designed for electronic component for elec parts or as substrates designed for electronic tronic circuits; or aquamarines. a. Metal windowsmachines, for X-ray or for bore-hole logging a. b. Oxide shapes in fabricated or semi-fabricated forms specially c. and of beryllium aluminium) in the form of emeralds (silicate Beryl other than calcium; impurities other than magnesium; b. boron. by weight of million per Containing than 10 parts less a. impurities metallic of by weight million per 200 parts than Containing less a. by weight; or greater % A purity of 99,99 b. Containing less than 10 ppm (parts per million) by weight of silver. of weight by million) per (parts ppm 10 than less b. Containing b. boron. by weight of million per Containing than 10 parts less beryllium compounds, beryllium of any and thereof, waste or scrap of manufactures Goods in the Military Controls. specified the foregoing, other than that CONTROLS. GOODS MILITARY ALSO N.B.: SEE a. Containing 000 less parts than per million 1 by weight of metallic following: the control not does Note: 1C230 1C228 Magnesium having both of the following characteristics: following the of both characteristics: having following 1C228 Magnesium the of both having 1C229 Bismuth 1C230 Beryllium metal, alloys containing more than 50 % beryllium by weight, by beryllium % 50 than more containing alloys metal, 1C230 Beryllium 1C227 Calcium having both of the following characteristics: characteristics: following the of both having 1C227 Calcium

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 79

Li) isotope to greater than its natural

GBq of tritium. GBq of

3 He), mixtures containing helium-3, and He), mixtures products or devices

3 1 g of helium-3. thickness of 0,10 mm or less. thickness of 0,10 1,48 × 10 containing any of the foregoing. than less containing device or product a control not does 2.C.18. Note: Item zirconium by weight, as follows: metal, alloys containing more than 50 % zirconium by weight, as follows: metal, alloys containing more than 50 zirconium by weight, compounds, manufactures thereof, waste or scrap of foregoing. the any of a having foil of form the in zirconium control not does 2.C.15. Note: Item 000, and products or devices to hydrogen tritium atoms exceeds 1 part in 1 containing any of the foregoing. than less containing device or product a control not does 2.C.17. Note: Item compounds containing more than 60 % hafnium by weight, manufactures % compoundsthan 60 containing more of any and foregoing. or scrap of the thereof, waste isotopic abundance and products or devices containing enriched lithium, as lithium, alloys, compounds,follows: elemental mixtures containing lithium, or scrap of any of the foregoing. waste thereof, manufactures dosimeters. thermoluminescent control not does 2.C.9. Note: Item Technical Note: isotopic abundance 6,5 approximately The natural is of lithium-6 weight percent (7,5 atom percent). 2.C.9. Lithium enriched in the lithium-6 ( lithium-6 the in enriched 2.C.9. Lithium 2.C.8. Hafnium metal, alloys containing more than 60 % hafnium by weight, hafnium weight, by hafnium % 60 than more containing alloys metal, 2.C.8. Hafnium 2.C.15. hafnium to 500 than 1 with a hafnium content of less part parts Zirconium 2.C.17. Tritium, tritium compounds, mixtures containing tritium in which the ratio of 2.C.18. Helium-3 ( 2.C.18. Helium-3

Li) isotope than its natural to greater

GBq (40 Ci) of tritium. of GBq (40 Ci)

He), mixtures containing helium-3, and products He), mixtures or devices

3 thickness of 0,10 mm or less. thickness of 0,10 helium-3. 1,48 × 10 tritium to hydrogen atoms exceeds 1 part in 1 000, and products or devices to hydrogen atoms exceeds 1 in 1 tritium part foregoing. the containing any of Note: 1C234 having does form of foil a not control zirconium in the Note: Technical Note: The natural isotopic abundance approximately 6,5 of lithium-6 is weight per cent (7,5 atom per cent). zirconium by weight, as follows: metal, alloys containing more than 50 % zirconium by weight, as follows: metal, alloys containing more than 50 zirconium by weight, compounds, thereof, waste or scrap of manufactures 0A001.f. in than those specified foregoing, other the any of hafnium compounds containing more than 60 % hafnium by % hafnium weight, manu hafnium compounds than 60 containing more of any and of the foregoing. thereof, waste or scrap factures of g 1 than less containing device or product a control not does Note: 1C232 isotopic abundance, and products or devices containing enriched lithium, as follows: elemental lithium, alloys, compounds, mixtures containing lithium, or scrap of any of the foregoing. waste thereof, manufactures dosimeters. thermoluminescent control not does Note: 1C233 Note: 1C235 does not control a product or device containing less than containing any of the foregoing. the containing any of 1C232 Helium-3 ( 1C232 Helium-3 1C235 Tritium, tritium compounds, mixtures containing tritium in which the ratio of 1C233 Lithium enriched in the lithium-6 ( lithium-6 the in enriched 1C233 Lithium 1C231 Hafnium metal, alloys containing more than 60 % hafnium by weight, by hafnium % 60 than more containing alloys metal, 1C231 Hafnium 1C234 than hafnium to 500 1 Zirconium with a hafnium content of less part parts

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 80

reaction: Actinium 225 Curium 244 Polonium 209 Actinium 227 253 Einsteinium Polonium 210 253 Californium 254 Einsteinium Radium 223 Curium 240 Gadolinium 148 Thorium 227 Curium 241 Plutonium 236 Thorium 228 Curium 242 Plutonium 238 Uranium 230 Curium 243 Polonium 208 Uranium 232 2.C.19. Radionuclides appropriate for making neutron sources based on alpha-n on based sources neutron making for appropriate 2.C.19. Radionuclides

GBq (100 millicuries) of activity. of millicuries) GBq (100 Actinium-225 Actinium-225 (Ac-225) Actinium-227 (Ac-227) Californium-253 (Cf-253) Curium-240 (Cm-240) Curium-241 (Cm-241) Curium-242 (Cm-242) Curium-243 (Cm-243) Curium-244 (Cm-244) Einsteinium-253 (Es-253) Einsteinium-254 (Es-254) Gadolinium-148 (Gd-148) Plutonium-236 (Pu-236) Plutonium-238 (Pu-238) Polonium-208 (Po-208) Note: 1C236 does not control a product or device containing less than 3,7 than less containing device or product a control not does Note: 1C236 reaction, other than those specified in 0C001 than those specified and other 1C012.a.,reaction, in the following forms: a. Elemental; b. Compounds having activity of 37 a total GBq/kg (1 Ci/kg) or greater; c. of 37 having GBq/kg Mixtures activity a total (1 Ci/kg) or greater; d. Products or devices containing any of the foregoing. Technical Note: In 1C236 ‘radionuclides’ are any of the following: — — — — — — — — — — — — — — 1C236 ‘Radionuclides’ appropriate for making neutron sources based on alpha-n on based sources neutron making for appropriate 1C236 ‘Radionuclides’

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 81

and having a

. ).

3 Ra), radium-226 alloys, compounds, mixtures

226 a. Medical applicators; a. Medical b. A product or device containing less than 0,37 GBq of radium-226. 3,7 GBq of activity 3,7 GBq of containing radium-226, manufactures thereof, and products or devices thereof, containing radium-226, manufactures containing any of the foregoing. following: the control not does 2.C.12. Note: Item In the following forms: In the a. Elemental; b. greater; kg or 37 GBq per of activity Compoundstotal having a c. greater; kg or 37 GBq per of activity total having a Mixtures d. Products or devices containing any of the foregoing. than less containing device or product a control not does 2.C.19. Note: Item m/s. 000 than 8 detonation velocity greater 6.C.1.o Any explosive with a crystal density greater than 1,8 g/cm 1,8 than greater density crystal a with explosive 6.C.1.o Any 2.C.12. Radium-226 ( 2.C.12. Radium-226 and having a detonation velocity and having a

). 2.C.6. Chlorine trifluoride (ClF trifluoride Chlorine ). 2.C.6.

3 Ra), radium-226 alloys, compounds, mixtures

226 of radium 226. a. Medical applicators; a. Medical millicuries) (10 GBq 0,37 than less containing device or product b. A Polonium-209 (Po-209) Polonium-210 (Po-210) Radium-223 (Ra-223) Thorium-227 (Th-227) Thorium-228 (Th-228) Uranium-230 (U-230) Uranium-232 (U-232) substances or mixtures containing more than 2 % by with weight thereof, a substances or mixtures containing more than 2 g/cm crystal density greater than 1,8 greater than 8 000 m/s. 000 greater than 8 containing radium 226, manufactures thereof, and products or devices and products or thereof, 226, containing radium manufactures foregoing. the containing any of — — — — — — — following: the control not does Note: 1C237 1C238 Chlorine trifluoride (ClF trifluoride 1C238 Chlorine 1C239 High explosives, other than those specified in the Military Goods Controls, or Controls, Goods Military the in specified those than other explosives, 1C239 High 1C237 Radium 226 ( 226 1C237 Radium

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 82 per

2 m measured by the ASTM B 330 μ

sheet or less. gaseous diffusion barriers see INFCIRC/254/Part 1 (as amended). (as 1 INFCIRC/254/Part see barriers gaseous diffusion powders; nickel a. Filamentary cm 000 1 of area an with sheets metal nickel porous b. Single standard; 1. A nickel purity content of 99,0 % or greater by weight; and or greater % 1. purity content of 99,0 A nickel 2. than 10 of less size A mean particle with an inside diameter between 100 and 300 mm; and with an between 100 inside diameter and 300 N.B.: For nickel powders which are especially prepared for the manufacture of manufacture the for prepared especially are which powders nickel N.B.: For characteristics: following the of both having powder a. Nickel 2.C.16.a. Item in specified materials produced from metal nickel b. Porous following: the control not does 2.C.16. Note: Item Technical Note: Item 2.C.16.b. to porous refers metal formed by compacting and sintering the pores intercon with fine 2.C.16.a. in Item material metal to form a material nected throughout the structure. of rhenium and tungsten containing 90 % by weight or more of any of rhenium and tungsten containing 90 combination of rhenium and tungsten, having both of the following character istics: segments) cylinder (including symmetry cylindrical hollow a with forms a. In kg. 20 than greater mass b. A 2.C.16. Nickel powder and porous nickel metal, as follows: as metal, nickel porous and powder 2.C.16. Nickel 2.C.20. % by rhenium; and weight or more alloys Rhenium, and alloys containing 90

per sheet or

2 m measured by American Society μ

less. a. Filamentary nickel powders; nickel a. Filamentary cm 000 1 of area an with sheets nickel porous b. Single for Testing and (ASTM) B330 Materials standard; segments) with an inside diameter between 100 and 300 mm; and between 100 and 300 with an inside diameter segments) 1. A nickel purity content of 99,0 % or greater by weight; and greater % or 1. purity content of 99,0 A nickel 10 than less of size particle mean 2. A Technical Note: 1C240.b.to porous refers metal formed by compacting and the sintering in 1C240.a. materials to form a with fine pores interconnected metal material structure. throughout the of rhenium and tungsten containing 90 % by of any weight or more of rhenium and tungsten containing 90 in 1C226, combination of rhenium and tungsten, than those specified other characteristics: following the having both of a. In forms with a hollow cylindrical symmetry (including cylinder kg. 20 than greater mass b. A as follows: characteristics: following the of both having powder a. Nickel 1C240.a. in specified materials from produced metal nickel b. Porous Note: 1C240 does not control the following: the control not does Note: 1C240 1C241 Rhenium, and alloys containing 90 % by weight or more rhenium; and alloys and rhenium; more or weight by % 90 containing alloys and 1C241 Rhenium, 1C240 Nickel powder and porous nickel metal, other than those specified in 0C005, in specified those than other metal, nickel porous and powder 1C240 Nickel

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 83

ore “programs” or “microprograms” or “microprograms” ore “programs” “production”, or “use” of any item contained in the List. This information may “production”, of any This information item contained in the List. or “use” take the form of “technical data” or “technical assistance”. “production”, or “use” of any item contained in the List. This information may “production”, of any This information item contained in the List. or “use” take the form of “technical data” or “technical assistance”. may “production”, of any This information item contained in the List. or “use” take the form of “technical data” or “technical assistance”. fixed in any tangible medium of expression fixed in any tangible medium of expression Nuclear Suppliers Group's as in control list INFCIRC/254/Rev.9/Part2 Nuclear Suppliers Group's as in control list INFCIRC/254/Rev.9/Part2 1.E.1. “Technology” – means information required for the “development”,specific 1.E.1. “Technology” – means information required for the “development”,specific 1.E.1. “Technology” – means information required for the “development”,specific 1.D.2. means of one a collection or “microprograms” or “software” more “programs” transit of dual-use items transit of dual-use items goods specified in 1A002, 1A007, 1A202, 1A225 to 1A227, 1B201, 1B225 1A227, 1B201, to 1A225 1A002, 1A007, 1A202, in specified goods 1C010.b., .b.4., 1C202, 1C210, 1C216, to 1B234, 1C225 1C002.b.3.or to 1D201. 1C241 or opment” or “production” of goods specified in 1A007, 1A202 or 1A225 to 1A227. opment” or “production” of goods specified in 1A007, 1A202 or 1A225 to 1A227. duction” or “use” of equipment specified in 1B001 duction” of equipment or “use” specified to 1B003.

1E201 “Technology” according to the General Technology Note for the “use” of “use” the for Note Technology General the to according 1E201 “Technology” 1E202 “Technology” according to the General Technology Note for the “devel the for Note “devel Technology the General for the Note to Technology according General 1E202 “Technology” the to according 1E203 “Technology” 1D201 “Software” specially designed for the “use” of goods specified in 1B201. 1.D.3. means of one a collection or “software” m 1D001 “Software” specially designed or modified for the “development”, “pro “development”, the for modified or designed specially 1D001 “Software” 2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and brokering exports, transfer, of control the for 5 Community 2009 of regime a up May 2009 setting 2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and brokering exports, transfer, of control the for 5 Community 2009 of regime a up May 2009 setting The corresponding Council No 428/ in systems, equipment Regulation (EC) and components identified as The corresponding Council No 428/ in systems, equipment Regulation (EC) and components identified as 1D Software 1E Technology M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 84

(8 l (litres)); and

(2 liters); and (2 liters); (2 liters); 3

3 3 );

3 );

2 );

2 ); or ); (150 ml) and 8 000 cm (50 ml) and 2 000 cm (50 ml) and 2 000 cm 3

3 O 3 3 O

2 ); 2

); 3

30 % Ti, 20 % W); % Ti, 20 30 of the following materials, having an overall impurity level of 2 % or of 2 level impurity having an overall following materials, the of less by weight: (CaF fluoride a. Calcium e. Hafnium oxide (hafnia) (HfO (hafnia) oxide e. Hafnium (ZrO (zirconia) oxide i. Zirconium d. Erbium oxide (erbia) (Er (erbia) oxide d. Erbium b. Calcium zirconate (metazirconate) (CaZrO (metazirconate) zirconate b. Calcium f. Magnesium oxide (MgO); oxide f. Magnesium % Nb, g. Nitrided niobium-titanium-tungsten alloy (approximately 50 (Y (yttria) oxide h. Yttrium c. Cerium sulfide (Ce sulfide c. Cerium weight; weight; and thereof. 1. A volume of between 50 cm 50 between of volume 1. A 2. Made or combination of or coated with any following of the materials, 1. A volume of between 150 cm 150 between of volume 1. A 2. by % or greater with tantalum, having Made of or lined purity of 99,9 a cm 50 between of volume 1. A 2. by % or greater Made of or lined with tantalum, having a purity of 98 3. Coated with tantalum carbide, nitride, boride, or any combination b. Crucibles having both of the following characteristics: following the of both having b. Crucibles a. Crucibles having both of the following characteristics: following the of both having a. Crucibles c. Crucibles having all of the following characteristics: Nuclear Suppliers Group's as in control list INFCIRC/254/Rev.9/Part2 2.A.1 Crucibles made of materials resistant to liquid actinide metals, as follows: as metals, actinide liquid to resistant materials of made 2.A.1 Crucibles and ;

); and CATEGORY 2 — MATERIALS PROCESSING — CATEGORY 2 3

3 ; ;

3 3 );

2 ); or

2 and 8 000 cm 000 and 8 ); );

and 2 000 cm 000 and 2 cm 000 and 2 3

O 3 3 O

2 ); ); 3

transit of dual-use items and 30 % Ti, 20 % W); weight; d. Erbium oxide (erbia) (Er (erbia) oxide d. Erbium e. Hafnium oxide (hafnia) (HfO (hafnia) oxide e. Hafnium thereof. b. Calcium zirconate (metazirconate) (CaZrO (metazirconate) zirconate b. Calcium of the following materials, having an overall impurity level of 2 % or having of the following an materials, overall impurity level of 2 less by weight: (CaF fluoride a. Calcium (MgO); oxide f. Magnesium Nb, % 50 (approximately alloy niobium-titanium-tungsten g. Nitrided (Y (yttria) oxide h. Yttrium weight; c. Cerium sulphide (Ce sulphide c. Cerium (ZrO (zirconia) oxide i. Zirconium 2. by or greater % having with tantalum, a purity of 98 Made of or lined 1. A volume of between 50 cm 50 between of volume 1. A 3. Coated with tantalum carbide, nitride, boride, or any combination 2. Made or combination of or coated with any of the following materials, 2. by greater % or Made with tantalum, having of or lined a purity of 99,9 cm 50 between of volume 1. A 1. A volume of between 150 cm 150 between of volume 1. A b. Crucibles having both of the following characteristics: following the of both having b. Crucibles c. Crucibles having all of the following characteristics: a. Crucibles having both of the following characteristics: following the of both having a. Crucibles 2A225 Crucibles made of materials resistant to liquid actinide metals, as follows: as metals, actinide liquid to resistant materials of made 2A225 Crucibles 2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and brokering exports, transfer, of control the for 5 Community 2009 of regime a up May 2009 setting The corresponding Council No 428/ in systems, equipment Regulation (EC) and components identified as Components and Equipment 2A Systems, M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 85

see Item 1.D.3. see Item nickel alloy containing more than 60 % nickel by weight. nickel alloy containing more than 60 Technical Note: nominal parameter diameter, the and size outlet inlet with different For valves 3.A.3.a. in Item to the smallest diameter. refers cutting metals, ceramics, or composites, which, according to the manufacturer's ceramics, cutting metals, technical specifications, can be equipped with electronic devices for simul axes: more two or in control” taneous “contouring “software”, associated their by controlled units control” “numerical N.B.: For a. mm or greater; of 5 A nominal size and seal; bellows a b. Having c. Wholly made of or lined with aluminium, aluminium alloy, nickel, or Nuclear Suppliers Group's as in control list INFCIRC/254/Rev.9/Part2 1.B.2. removing or for follows, and any Machine tools, as combination thereof, 3.A.3. Valves having all of the following characteristics: following the of all having 3.A.3. Valves

and

transit of dual-use items manufacture of any of the following: camshafts; or a. Crankshafts cutters; or b. Tools worms; c. Extruder manufacture of gears. For such machines see 2B003. machines see such gears. For manufacture of nickel alloy containing more than 60 % nickel by weight. nickel alloy containing more than 60 ceramics or “composites”, which, according to the manufacturer's technical “numerical for devices electronic equipped with be can specification, follows: as control”, Note 2: 2B001 does not control special purpose machine tools limited to the to limited tools machine purpose special control not Note 2: does 2B001 c. Wholly made of or lined with aluminium, aluminium alloy, nickel, or nickel, alloy, aluminium aluminium, with lined or of made c. Wholly 2B201. ALSO N.B.: SEE the to limited tools machine purpose special control not Note 1: does 2B001 a. mm or greater; of 5 size’ A ‘nominal seal; bellows a b. Having Technical Note: and in diameters, the ‘nominal inlet outlet size’ For valves with different diameter. smallest the to 2A226 refers 2B001 Machine tools and any combination thereof, for removing (or cutting) metals, cutting) (or removing for thereof, combination any and tools 2B001 Machine 2A226 Valves having all of the following characteristics: following the of all having 2A226 Valves 2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and brokering exports, transfer, of control the for 5 Community 2009 of regime a up May 2009 setting The corresponding Council No 428/ in systems, equipment Regulation (EC) and components identified as Equipment Production and Inspection 2B Test, M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 86 m according to ISO 230/2 m according to ISO μ

machining only bar feed thru, maximum is equal to if bar diameter of mounting is no mm and capability there chucks. or less than 42 machining for capabilities and/or milling have drilling Machines may mm. less than 42 parts with diameters (1988) along any linear axis (overall positioning) for machines capable of machines positioning) for (overall axis (1988) along any linear mm; than 35 greater machining diameters compensations available better (less) than 6 (less) better compensations available Note: Item 1.B.2.a. does not control bar machines (Swissturn), limited to a. Machine tools for turning, that have “positioning accuracies” with all

m along one or more linear axis; and axis; m along one or more linear μ

for part programming data input; and m along one or more linear axis; and axis; m along one or more linear μ producing contact lenses, having all of the following: the of all having lenses, producing contact software based ophthalmic using to limited controller a. Machine b. No vacuum chucking. vacuum b. No simultaneously for “contouring control”; simultaneously for than 1,1 d. Engraved or facetted jewellery parts; or parts; jewellery facetted or d. Engraved prostheses. e. Dental grinding capabilities (e.g., a turning machine with milling capa milling turning machine with a (e.g., grinding capabilities bility), must be evaluated against each applicable entry 2B001.a., b. or c. touring control”; coordinated be can which axis one rotary plus axes linear b. Three 1,1 a. “Unidirectional positioning repeatability” equal to or less (better) less or to equal repeatability” positioning a. “Unidirectional 2. Two or more axes which can be coordinated simultaneously for “con for simultaneously coordinated be can which axes more or 2. Two 1. “Unidirectional positioning repeatability” equal to or less (better) than (better) less or to equal repeatability” positioning 1. “Unidirectional for designed specially machines turning control not does Note: 2B001.a. following: the of all 1. Having Note 3: A machine tool having at least two of the three turning, milling or turning, milling Note 3: three the two of least having at tool machine A 2B002. see machines, finishing optical N.B.: For following: the of all having turning for tools a. Machine following: the of any having milling for tools b. Machine

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m along one or more linear axis; or axis; linear more m along one or μ

m along one or more linear axis with a travel length m along one or more linear axis with a travel length m (along one or more linear axis with a travel length μ μ μ 2B001.b.2.d. and mm of travel; TIR over 300 than 2 seconds of arc, (better) than 1,1 m; less than 1 than 1,4 m; than 4 m and less than 1 greater to or equal than 6,0 m; or than equal to 4 or greater Technical Note: having machine tool a is mechanism machine tool’ ‘parallel A multiple rods which are linked with a platform and actuators; rod simultaneously respective actuators operates the each of the and independently. equal to or less (better) than 1,1 (better) equal to or less a. mm TIR; than Spindle 0,0004 “run-out” and “camming” less (better) b. Angular deviation of slide movement (yaw, pitch and roll) less touring control” having any of the following; having touring control” any the of in specified are tools’ machine mechanism N.B.: ‘Parallel (better) less or to equal repeatability” positioning a. “Unidirectional equal positioning b. “Unidirectional to or repeatability” less (better) (better) less or to equal repeatability” positioning c. “Unidirectional tool’; machine mechanism ‘parallel a d. Being 3. A “unidirectional positioning repeatability” for jig boring machines, jig for positioning repeatability” A “unidirectional 3. following: the of all having machines cutting 4. Fly 2. Five or more axes which can be coordinated simultaneously for “con for simultaneously coordinated be can which axes more or 2. Five

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m μ

m along one or more linear axis with a travel length m along one or more linear axis with a travel length m along one or more linear axis with a travel length m along one or more linear axis; and axis; m along one or more linear μ μ μ μ diameter or length. machines, having all of the following: the machines, having of all and grinding; cylindrical to 1. Limited outside mm 150 of capacity workpiece maximum a to 2. Limited or a waxis, a z-axis with a “unidirectional positioning repeat than 1,1 less (better) ability” “contouring control”; or control”; “contouring than 1,1 m; less than 1 than 1,4 or m; than 4 m and less than 1 greater to or equal than 6,0 m. equal to than 4 or greater than 1,1 a. Cylindrical external, internal, and a. Cylindrical grinding external-internal have not do that grinders jig as specifically designed b. Machines b. Three or more axes which can be coordinated simultaneously for simultaneously coordinated be can which axes more or b. Three following: having touring control” any the of (better) less or to equal repeatability” positioning a. “Unidirectional equal positioning b. “Unidirectional to or repeatability” less (better) (better) less or to equal repeatability” positioning c. “Unidirectional a. “Unidirectional positioning repeatability” equal to or less (better) less or to equal repeatability” positioning a. “Unidirectional 2. Five or more axes which can be coordinated simultaneously for “con for simultaneously coordinated be can which axes more or 2. Five 1. Having all of the following: the of all 1. Having Note: 2B001.c. does not control grinding machine as follows: c. Machine tools for grinding having any of the following: the of any having grinding for tools c. Machine

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ruments, or systems, as follows: or systems, ruments, m within a measuring range up to 0,2 mm; up m within a measuring range to 0,2 μ better (less) than 0,2 1. Non-contact type measuring systems with a “resolution” equal to or

1.B.3. 1.B.3.b. b. Linear displacement measuring instruments, as follows: as instruments, measuring displacement Linear 1.B.3.b. b.

controlled in 2B006.b.1.c. c. Surface grinders. c. Surface additives; a. Water or other liquid jets, including those employing abrasive or beam; b. Electron and beam; c. “Laser” and control”; “contouring for simultaneously coordinated be a. Can 0,003°; than (better) less of “accuracy” positioning b. A Note: Displacement measuring “laser” interferometers are only two or more rotary axes which can be coordinated simultaneously for rotary two or more control”; “contouring following: of the 1. by Removing means of any of the following: material following: the of all having axes rotary two least 2. At m. drilling, having a maximum depth-of-bore capability exceeding 5 assemblies”, as follows: as assemblies”, d. Electrical discharge machines (EDM) of the non-wire type which have which type non-wire the of (EDM) machines discharge d. Electrical all having “composites”, or ceramics metals, removing for tools e. Machine f. machines and turning deep-hole- machines modified for Deep-hole-drilling 2B006 Dimensional inspection or measuring systems, equipment and “electronic 2B006.b. Linear and angular displacement measuring instruments, as follows: 1.B.3. 1.B.3. Dimensional inspection machines, inst follows: machines, as inspection instruments, Dimensional 1.B.3. 1.B.3. measuring displacement angular and 2B006.b. Linear 2B006.b. 1. ‘Linear displacement’ measuring instruments having any of the following: the of any having instruments measuring displacement’ ‘Linear 2B006.b. 1.

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 90 m or better; and m or better; μ

m (L is the measured length in millimeters); length in measured is the m (L μ systems, without closed or open loop feedback, containing a laser to measure slide movement errors of machine tools, dimen equipment. sional inspection machines, or similar the full operating range, for LVDTs with an operating range up to range an operating with LVDTs for range, operating full the 5 mm; or 5 mm for LVDTs with an operating range greater than 5 mm; and 000) (0,2 + L/2 2. 0 % measured from to than 0,1 (better) equal to or less “Linearity” ± 1 room temperature ambient test K; and around a standard pressure: a standard temperature 0,1 of scale full their over “resolution” 1. A 2. than (less) equal to or better uncertainty” With a “measurement the following characteristics: a. 1. 0 % measured from to than 0,1 (better) equal to or less “Linearity” % per day at a standard than 0,1 (less) equal to or better Drift b. and laser; a a. Contain K 1 ± of range temperature a over hours, 12 least at for b. Maintain interferometer measuring control not 1.B.3.b.3. does Note: Item 2. Linear variable differential transformer (LVDT) systems having both of both having systems (LVDT) transformer differential variable 2. Linear characteristics: following the of both having systems 3. Measuring Technical Note: 1.B.3.b. means In Item the change displacement’ of distance between ‘linear probe the measuring and the measured object. and

m or less (better); m or μ

VDT) systems having of all VDTs with a ‘full operating range’ with a ‘full VDTs or

and VDTs with a ‘full operating range’ greater than ± greater operating range’ ‘full a with VDTs m within a measuring range up to 0,2 mm; up a measuring range m within to 0,2 μ and ariable Differential Transformer (L Transformer ariable Differential the ‘full operating range’, for L the ‘full mm; 5 and including ± up to 5 mm for L 5 mm; a. 0 to than 0,1 % measured from (better) equal to or less “Linearity” test room ± temperature 1 K; b. 0 to than 0,1 % measured from (better) equal to or less “Linearity” the following: 0,1 of scale full their over “resolution” a. A the following: following: the of any 1. Having 2. than 0,1 % per day at a standard ambient (better) equal to or less Drift “laser”; a 1. Containing (better) than 0,2 2. Maintaining, for at least 12 hours, at a temperature of 20 ± 1 °C, all of all °C, 1 ± 20 of temperature a at hours, 12 least at for 2. Maintaining, Technical Note: For the purposes of 2B006.b.1.b., operating half of the range’is ‘full total possible linear displacement of the LVDT. For example, LVDTs operating mm with a ‘full range’up to and can measure a including ± 5 mm. total possible linear displacement of 10 b. Linear V b. Linear c. following: Measuring systems having of the all a. Non-contact type measuring systems with a “resolution” equal to or less or to equal “resolution” a with systems measuring type a. Non-contact Technical Note: For the purpose of 2B006.b.1. ‘linear displacement’ means the change of distance between the measuring probe and the measured object.

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mators, using collimated light (e.g., laser light) to detect angular displacement of a mirror. a digital control a digital and deviation” equal to or better (less) than 0,00025°; (less) deviation” equal to or better acteristics: acteristics: incorporating and techniques control loop closed or feedback 1. Employing 2. unit; Hz; 000 2 and 20 between more or RMS g 10 at vibrating of 3. Capable 4. of Capable 50 of imparting forces measured “bare table”; kN or greater being and kHz 5 than bandwidth greater real-time a with testing, vibration 1.B.6.a.; Item in specified system a designed for capable of imparting 1.B.6.a.; in systems specified Item Note: Item 1.B.3.c. does not control optical instruments, such as autocolli such as instruments, 1.B.3.c. optical does not control Item Note: a. Electrodynamic vibration test systems, having all of the following char following the of all having systems, test vibration a. Electrodynamic for designed specially “software” with combined units, control Digital b. amplifiers, associated without or with units), (shaker thrusters Vibration c. d. of 50 a force which measured “bare table”, kN usable are for the or greater 1.B.6. Vibration test systems, equipment, and components as follows: as components and equipment, systems, test 1.B.6. Vibration 1.B.3.c c. Angular displacement measuring instruments having an “angular position “angular an having instruments measuring displacement Angular 1.B.3.c c.

m (L is the measured length in mm) m (L is the measured

or (better) than (0,2 + L/2 000) at any point within a measuring range, when compensated for the refractive index of air; mators, using collimated light (e.g., laser light) to detect angular detect to light) laser (e.g., light mators, using collimated a mirror. displacement of b. equal to or less uncertainty” Capable of achieving a “measurement Technical Note: In 2B116.b., control bandwidth’‘real-time means the maximum rate at sampling, of processing cycles complete can execute which a controller data and control signals. transmitting than 50 equal to or greater kN, a force measured capable of imparting in 2B116.a.; specified systems test and usable in vibration table’, ‘bare “accuracy” equal to or less (better) than 0,00025°; equal to or less (better) “accuracy” capable of vibrating a system at an controller, incorporating a digital acceleration equal to or than 50 kN, measured greater equal to or forces imparting kHz while greater than 10 g rms table’; ‘bare between 20 Hz and 2 software, with control bandwidth’a ‘real-time greater than 5 kHz 2B116.a.; in specified systems test vibration with use designed for Note: 2B006.b.2. instruments, such as autocolli does not control optical c. Vibration thrusters (shaker units), with or without associated amplifiers, associated without or with units), (shaker thrusters c. Vibration a. Vibration test systems employing feedback or closed loop techniques and techniques loop closed or feedback employing systems test a. Vibration b. Digital controllers, combined with specially designed vibration test 2B116 Vibration test systems, equipment and components therefor, as follows: as therefor, components and equipment systems, test 2B116 Vibration 2B006.b. 2. Angular displacement measuring instruments having an angular position angular an having instruments measuring displacement Angular 2B006.b. 2.

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or cutting metals, ceramics, or composites, which, ceramics, according to or cutting metals, the manufacturer's technical specifications, can be equipped with electronic axes: more simultaneous “contouring in two or control” devices for see Item 1.D.3. see Item multiple shaker units into a complete shaker system capable of providing multiple an effective combined force of 50 kN or greater, measured “bare table”, which are usable for the systems specified in Item 1.B.6.a. Technical Note: 1.B.6. In Item “bare table” means table, or a or surface, with no flat fixtures fittings. e. d. Test piece support structures and electronic units designed to combine to designed units electronic and structures support piece Test e. d. N.B.: For “numerical control” units controlled by their associated “software”, “software”, associated their by controlled units control” “numerical N.B.: For 1.B.2. 1.B.2. Machine tools, as follows, and any combination thereof, for removing for thereof, combination any and follows, as tools, Machine 1.B.2. ; )

1 ( or national )

1 (

standard;

) 1 (

multiple shaker units in a system capable of providing an effective table’, ‘bare than 50 kN, measured greater equal to or combined force in 2B116.a. systems specified and usable in vibration method of calculating the accuracy value is described in the ISO 230/2 (1988) becomes the stated ‘positioning accuracy’ of each axis for the model (Âx for the of each axis ‘positioning accuracy’becomes the stated Ây...); axes; are linear there as values accuracy’ ‘positioning equivalents may be used for each machine tool model if provided to, and may be used for each machine tool model if equivalents accepted by, national authorities instead of individual machine Stated tests. follows: as derived be to are accuracy’ ‘positioning 1. machines of a five model to be evaluated; Select 230/2 (1988) ISO according to accuracies axis linear the 2. Measure 2B001, as follows, for removing or cutting metals, ceramics or “composites”, 2B001, removing ceramics or cutting metals, as follows, for can be specification, technical which, according to the manufacturer's in “contouring control” simultaneous for devices electronic equipped with axes: two or more Technical Notes: derived under Stated ‘positioning levels the following procedures accuracy’ from measurements made according to ISO 230/2 (1988) of each machine. The for each axis 3. (A) accuracy values the Determine d. Test piece support structures and units designed electronic to combine Technical Note: In 2B116, ‘bare table’ means a flat table, or surface, with no or fixture fittings. 4. average value This each axis. of value average accuracy the Determine stated many as be will there axis, linear each to refers 2B201 Item 5. Since 2B201 in specified than those other and any combination thereof, tools Machine

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m according to ISO 230/2 (1988) μ m according to ISO 230/2 m according to ISO axis (overall (1988) along any linear μ 30 following characteristics: and m; 2 than greater travel 1. X-axis than (more) worse x-axis the on accuracy” “positioning 2. Overall than 6 positioning); touring control”. 1. “Positioning accuracies” with all compensations available better (less) better available compensations all with accuracies” 1. “Positioning 2. Two or more contouring rotary axes; or “con for simultaneously coordinated be can which axes more or 3. Five the of both having machines milling control not does 1.B.2.b. Note: Item 1.B.2.b b. Machine tools for milling, having any of the following characteristics: ) or national

1 , then the builder , then the )

1 m or better (less) for (less) m or better μ ( and or m or better (less) for milling and for milling turning (less) m or better μ

m according to ISO 230/2 (1988) ( m according to ISO 230/2 (1988) μ

μ 30

b. Overall ‘positioning accuracy’ on the x-axis more (worse) than (worse) more x-axis the on accuracy’ ‘positioning b. Overall characteristics: m; 2 than greater travel a. X-axis manufacture of any of the following parts: a. Gears; camshafts; or b. Crankshafts cutters; or c. Tools worms. d. Extruder grinding capabilities (e.g., a turning machine with milling capa milling turning machine with a (e.g., grinding capabilities bility), must be evaluated against each applicable entry 2B201.a., b. or c. touring control”; less (better) than 6 less (better) equivalents along any axis; linear Note: 2B201.a. does not control milling machines having the following the having machines milling control not Note: 2B201.a. does 3. Five or more axes which can be coordinated simultaneously for “con for simultaneously coordinated be can which axes more or 3. Five 2B201.c.. has a stated ‘positioning accuracy’ of 6 of accuracy’ ‘positioning stated a 2B201.c.. has grinding machines, and 8 230/2 (1988) machines, both ISO according to or to equal available” compensations “all with accuracies’ 1. ‘Positioning 2. Two or more contouring rotary axes; rotary contouring more or 2. Two should be required to reaffirm the accuracy level once every eighteen every once level accuracy the reaffirm required to should be months. Note 1: 2B201 does not control special purpose machine tools limited to the to limited tools machine purpose special control not Note 1: does 2B201 6. If any axis of a machine tool not controlled by 2B201.a., 2B201.b. or by controlled not tool machine a of axis any 6. If or turning, milling Note 2: three the two of least having at tool machine A 2B201. a. Machine tools for milling, having any of the following characteristics: characteristics: following the of any having milling, for tools Machine 2B201. a.

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diameter or length; and m according to ISO 230/2 m according to ISO axis (overall (1988) along any linear μ a. Limited to a maximum workpiece capacity of 150 mm outside mm 150 following characteristics: the machines having all of capacity workpiece maximum a to a. Limited c. and z x, to limited b. Axes Positioning microns. 4 than (better) less positioning accuracy accuracy is according to ISO 230/2 (1988). 1. Cylindrical external, internal, and external-internal grinding 2. Jig grinders that do not have a z-axis or w-axis with an overall than 4 positioning); touring control”. 1. “Positioning accuracies” with all compensations available better (less) better available compensations all with accuracies” 1. “Positioning “con for simultaneously coordinated be can 2. which Two or more contouring rotary axes; or axes more or 3 Five follows: as machines grinding control not does 1.B.2.c. Note: Item 1.B.2.c c. grinding, having following characteristics: Machine tools for any of the m m μ μ ) or national

along any linear axis )

1 ( or national equivalents. )

1 (

or and m according to ISO 230/2 (1988) ( m according to ISO 230/2 (1988) μ

limited to machining only bar feed thru, if maximum and there mm than 42 less or equal to is bar diameter is no capability of mounting chucks. Machines may have drilling and/or for milling capabilities machining parts mm. than 42 with diameters less diameter or length; 2. Axes limited to x, z and c; and z x, to limited 2. Axes than 4 overall ‘positioning (better) accuracy’ less (1988) 230/2 ISO according to machines having all of the following characteristics: the of machines having all 1. mm outside Limited to a maximum workpiece capacity of 150 Note: 2B201.c. does not control bar machines (Swissturn), with “all compensations available” better (less) than with “all compensations 6 (less) available” better 230/2 (1988) ISO according to (overall positioning) for machines capable of machining mm; diameters greater than 35 b. Jig grinders that do not have a z-axis or a w-axis with an or a w-axis do not have a z-axis Jig grinders that b. a. Cylindrical external, internal, and external-internal grinding c. Machine tools for turning, that have ‘positioning accuracies’ ‘positioning have that turning, for tools c. Machine touring control”; less (better) than 4 less (better) equivalents along any axis; linear Note: 2B201.b. does not control grinding machines as follows: as machines grinding control not does Note: 2B201.b. 3. Five or more axes which can be coordinated simultaneously for “con for simultaneously coordinated be can which axes more or 3. Five 2. Two or more contouring rotary axes; rotary contouring more or 2. Two 1. ‘Positioning accuracies’ with “all compensations available” equal to or to equal available” compensations “all with accuracies’ 1. ‘Positioning 2B201 b. Machine tools for grinding, having any of the following characteristics: following the of any having grinding, for tools Machine 2B201 b.

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equal to

0, MPE , equal to or less(better) , equal to or 0zMPE m (where L is the measured L is the m (where μ

or E

0y MPE , E m (where L is the measured length in mm) at length in mm) the measured L is m (where μ 0x MPE or greater; and or greater; pressurizing a closed cavity through various media (gas, liquid, cavity pressurizing a closed equal pressure directions to create in all particles, etc.) solid upon cavity a workpiece or material. within the working pressure and the working temperature which both the in are achieved and does That not include dimension fixtures. will be the smaller of either inside diameter pressure chamber or the inside diameter of the insulated furnace chamber, depending on which of the two chambers is located inside the other. 1. Capable of achieving a maximum working of 69 pressure MPa mm; 152 of excess in diameter inside an with cavity chamber 2. A 1.B.5.a. in Item specified presses” Technical Notes: 1. In Item 1.B.5. “Isostatic presses” means equipment capable of 2. In Item 1.B.5. the inside chamber dimension is that of the chamber a. “Isostatic presses” having both of the following characteristics: following the of both having presses” a. “Isostatic b. Dies, molds, and controls specially designed for the “isostatic or less (better) than (1,7 + L/800) (better) or less machine at any point operating range of the length mm) within the in (i.e., within the length of the axis), according to ISO 10360-2(2009). than (1,25 + L/1 000) than (1,25 + L/1 within the any the machine (i.e., point of within the operating range 10360-2(2009); to ISO according or the axis), length of (E measurement length of error maximum permissible length measurement along any axis (one dimensional), identified as along any axis (one dimensional), identified length measurement E any combination of 2. Three or more axes and having a three dimensional (volumetric) machines (CMM) having of the following characteristics: machines (CMM) either 1. Having only two axes and having a maximum permissible error of 1.B.3. 1.B.3. Dimensional inspection machines, instruments, or systems, as follows: 1.B.5. 1.B.5. follows: equipment, as and related presses”, “Isostatic 1.B.3.a Computer controlled coordinate measuring controlled or numerically a. or ) equal to

0,MPE , equal to or less 0z,MPE , or E , or m (where L is the measured length m (where μ m (where L is the measured length L is the measured m (where 0y,MPE μ , E 0x,MPE

and

greater; length measurement along any axis (one dimensional), identified as along dimensional), identified any axis (one length measurement E any combination of or less (better) than (1,7 + L/800) or less (better) (better) than (1,25 + L/1 000) (better) than (1,25 + L/1 in mm) at any point within the operating range of machine (i.e., according to ISO 10360-2(2009); within the length of axis), maximum permissible error of length measurement (E measurement length of error maximum permissible in mm) at any point within the operating range of machine (i.e., according to ISO 10360-2(2009); within the length of axis), 1. Capable of achieving of 69 a maximum working MPa or pressure 1. 2. A chamber cavity with an inside diameter in excess of 152 mm; 2. in excess of 152 cavity with an inside diameter A chamber specified in 2B204.a. machines (CMM) having either of the following characteristics: machines (CMM) having either 1. Having only two axes and having a maximum of permissible error 2. Three or more axes and having a three dimensional (volumetric) specified in 2B006, as follows: Technical Note: In 2B204 the inside chamber dimension is that of the chamber in which both the working temperature and the working pressure are achieved and does not the inside That either dimension of be the smaller include fixtures. will diameter of the pressure chamber or the inside diameter of insulated furnace chamber, depending two on located inside the chambers which of is the other. equipment, as follows: equipment, as characteristics: following the of both having presses” a. “Isostatic b. Dies, moulds and controls, specially designed for “isostatic presses” 2B206 Dimensional inspection machines, instruments or systems, other than those than other systems, or instruments machines, inspection 2B206 Dimensional 2B204 “Isostatic presses”, other than those specified in 2B004 or 2B104, and related and 2B104, or 2B004 in specified those than other presses”, 2B204 “Isostatic 2B206. a. Computer controlled or numerically controlled coordinate measuring coordinate controlled numerically or controlled Computer 2B206. a.

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 96 m μ

m per 5 mm; and mm; m per 5 μ of the most accurate configuration of the CMM specified

0, MPE than 3,5

both of the following characteristics: the both of 1. “Measurement along uncertainty” any linear axis equal to or better (less) 0,02°. than less or to equal deviation” position 2. “Angular according to ISO 10360-2(2009) by the manufacturer (e.g., best of the following: probe, stylus length, motion parameters, environment) and with all compensations available shall be compared to the 1,7 + L/ 800 threshold. Technical Note: The E effectors’ having either of the following characteristics: 1. Specially having either of the following characteristics: effectors’ to handling designed standards applicable to comply national safety with high explos for code ratings electrical meeting example, high explosives (for ives); 1.B.3.d d. Systems for simultaneous linear-angular inspection of hemishells, having hemishells, of inspection linear-angular simultaneous for Systems 1.B.3.d d. 1.A.3.a1 ‘Robots’, ‘end-effectors’ and control units as follows: a. ‘Robots’ or ‘end- or ‘Robots’ a. follows: as units control and ‘end-effectors’ 1.A.3.a1 ‘Robots’, m μ

and m per 5 mm; m per 5 μ of the most accurate configuration of the CMM specified

controlled if they meet or exceed the criteria specified for the specified or controlled if they meet exceed the criteria measuring machine function. the function or machine tool threshold anywhere within its operating range. threshold anywhere within its 0,MPE (better) than 3,5 2. “Angular position deviation” equal to or less than 0,02°. than less or to equal deviation” position 2. “Angular both of the following characteristics: following the both of 1. “Measurement uncertainty” along any linear axis equal to or less safety standards applicable to handling high explosives (for example, high code ratings for explosives); meeting electrical Technical Notes: parameters of measurement All values in 2B206 represent plus/minus i.e., not total band. 2B007, as follows: 2B007, as designed to comply with national specially a. “Robots”or “end-effectors” Technical Note: The E Note 1: Machine tools that can be used as measuring machines are according to ISO 10360-2(2009) by the manufacturer (e.g., best of the of best 10360-2(2009) manufacturer (e.g., ISO according to by the following: probe, stylus, length, motion parameters, environments) and with all compensations available shall be compared to the 1,7 + L/800 threshold. Note 2: A machine specified in 2B206 is controlled if it exceeds the control 2B207 “Robots”, “end-effectors” and control units, other than those specified in specified those than other units, control and “end-effectors” 2B207 “Robots”, 2B206. b. Systems for simultaneous linear-angular inspection of hemishells, having hemishells, of inspection linear-angular simultaneous for Systems 2B206. b.

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controllable; phenomenon, the output of which (after conversion into a signal that phenomenon,conversion into a the output which (after of by can be interpreted a control unit) is able to generate “programs” or “program” data. This numerical or modify programmed instructions imaging, acoustical vision, infrared machine with “sensors” includes or acoustic position measuring, optical inertial feel, imaging, tactile torque measuring capabilities. or force ranging or by “programs” modify allowing or a user to insert, replace facility means other than: or interconnections; or wiring in change physical (a) a (b) including of function controls entry of parameters. the setting (a) Manipulation mechanisms which are only manually/teleoperator industrial applications such as automobile paint-spraying booths. may be of the continuous path or of the point-to-point variety, may use the continuous variety, may be of of the point-to-point path or multifunctional; is (a) of the following and characteristics: “sensors”, has all parts, tools, or special is capable of positioning (b) material, or orienting incor (c) space; devices through movements in three-dimensional variable porates three or more closed or open loop servo-devices which may include by means programmability” “user-accessible has and (d) stepping motors; method of teach/playback computer which or by means of an electronic inter i.e., without mechanical logic controller, may be a programmable vention. specified in Item 1.A.3.a. non-nuclear for designed specially ‘robots’ control not does 1.A.3. Note: Item Technical Notes: 1. 1.A.3. ‘Robots’ In Item ‘robot’ means a manipulation mechanism, which of a physical In the above means detectors definition “sensors” N.B.1: the means programmability” “user-accessible definition above the N.B.2: In devices: following the include not does definition above N.B.3: The 1.A.3.b Control units specially designed for any or ‘end-effectors’ of the ‘robots’ specified in 2B207.a. b. Control units designed specially for any of the “robots” or “end-effectors”

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moving devices operating according to mechanically fixed according to mechanically moving operating devices by limited programmed motions. The “program” is mechanically fixed stops, such as pins or cams. The sequence of motions and the changeable by or not variable paths or angles are of selection means; electrical or electronic, mechanical, automated moving anisms which are devices operating according programmed motions. The is fixed “program” to mechanically pins stops such as but adjustable, by fixed, limited mechanically or cams. The sequence of motions of paths or and the selection within the fixed “program” pattern. Variations angles are variable (e.g., of the “program” changes pattern or modifications of pins or accomplished motion in one exchanges axes are or more of cams) operations; only through mechanical automated moving which are devices, operating according to programmed motions. The “program” is fixed mechanically variable but the sequence proceeds only by the binary signal binary devices from mechanically fixed or electrical adjustable stops; bins of storage array of a vertical part as an integral manufactured or storage those bins for the contents of and designed to access retrieval. 2. In ‘End-effectors’ Item 1.A.3. are ‘end-effectors’ is tooling that and any other tooling units’, ‘active grippers, to the baseplate on arm. manipulator attached the end of a ‘robot’ (b) Fixed sequence manipulation mechanisms which are automated (c) Mechanically controlled variable sequence manipulation mech (d) Non-servo-controlled variable sequence manipulation mechanisms systems manipulator coordinate Cartesian as defined cranes (e) Stacker motive power, process energy or sensing to the workpiece. N.B.: In the above definition ‘active tooling units’ is a device for applying for device a is units’ tooling ‘active definition above the N.B.: In

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 99

designed to deform metal plus two auxiliary rollers which support the which rollers auxiliary two plus metal deform designed to process. in the deformation directly but do mandrel, not participate equipped with “numerical control” units or a computer control; equipped with “numerical 0,010 kg × mm/kg per plane; and a. or guiding); and (active rollers or more Three be can specification, technical manufacturer's the to according b. Which, mm. between 75 diameter and 400 having a length of 600 mm or more and having all of the following more and char of the having mm or all having length of 600 a acteristics: mm; 75 than greater diameter journal or 1. Swing and kg; 23 to 0,9 from of capability 2. Mass 000 rpm; 3. than 5 Capable of balancing speed of revolution greater rotor components and having all of the following characteristics: mm; 75 than greater diameter 1. Journal kg; 23 to 0,9 from of capability 2. Mass than equal to or less imbalance Capable of balancing to a residual 3. type. drive 4. Belt tions, and as follows: mandrels, characteristics: following the of both having 1. Machines 2. Rotor-forming mandrels designed to form cylindrical rotors of inside Note: Item 1.B.1.a. includes machines which have only a single roller vertical, as follows: rotors balancing flexible balancing machines designed for Centrifugal a. cylindrical hollow balancing for designed machines balancing b. Centrifugal 3.B.3. Centrifugal multiplane balancing machines, fixed or portable, horizontal or horizontal portable, or fixed machines, balancing multiplane 3.B.3. Centrifugal 1.B.1. Flow-forming machines, spin-forming machines capable of flow-forming func flow-forming of capable machines spin-forming machines, 1.B.1. Flow-forming

and and

and 0,01 kg × mm/kg per plane; equipped control” units or a computer control; with “numerical to deform metal plus which two auxiliary rollers support the mandrel, in the deformation process. but do directly not participate diameter between 75 mm and 400 mm. mm and 400 diameter between 75 having a length of 600 mm or more and following mm or more having of the all having length a of 600 characteristics: mm; 75 than greater diameter journal or 1. Swing kg; 23 to 0,9 from of capability 2. Mass 1. or guiding); (active or more rollers Three be can specification, technical manufacturer's the to according 2. Which, 3. Capable of balancing speed of revolution greater than 5 000 r.p.m.; than 5 balancing speed revolution greater 3. Capable of of rotor components and having all of the following characteristics: mm; 75 than greater diameter 1. Journal kg; 23 to 0,9 from of capability 2. Mass than equal to or less imbalance Capable of balancing to a residual 3. 4. Belt drive type. drive 4. Belt b. Rotor-forming b. Rotor-forming mandrels designed to form cylindrical rotors of inside vertical, as follows: a. Centrifugal balancing machines designed for balancing flexible rotors functions, other than those specified in 2B009 2B109, than those specified or functions, other and mandrels, as follows: a. Machines having both of the following characteristics: Note: 2B209.a. includes machines which have only a single roller designed b. balancing hollow cylindrical balancing machines designed for Centrifugal 2B219 Centrifugal multiplane balancing machines, fixed or portable, horizontal or horizontal portable, or fixed machines, balancing multiplane 2B219 Centrifugal 2B209 Flow forming machines, spin forming machines capable of flow

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 100 ; and

of semiconductor wafers. (1 700 °C); 2. Capable of operating with melting temperatures above 973 1 K 1. Capable of operation at temperatures above 1 123 K (850 °C); (850 K 123 1 above temperatures at operation of 1. Capable and diameter; in less or mm 600 coils 2. Induction kW or more; 3. power Designed inputs for of 5 processing the for designed furnaces control not does 1.B.4.a. Note: Item 1.B.4.a. Item in specified furnaces designed for operation); or operation); 0,6 m or more (over-the-wall operation). istics: istics: cm 000 20 and 000 1 between capacities electrode 1. Consumable supplies therefor, as follows: as supplies therefor, characteristics: following the of all having a. Furnaces b. kW or more, specially output Power supplies, with a specified power of 5 chemical separation operations or hot cells, having either of the following characteristics: a. wall (through-the-wall of hot m or more cell 0,6 of penetrating A capability b. of bridging A capability wall with a thickness of over the top of a hot cell Technical Note: of human a actions to Remote manipulators provide operator translation remote operating arm and fixture. They terminal may be of a master/slave type or operated by joystick or keypad. furnaces and related equipment, as follows: equipment, as and related furnaces character following the of both having furnaces casting and remelt a. Arc 1.B.4. Controlled atmosphere (vacuum or inert gas) induction furnaces, and power and furnaces, induction gas) inert or (vacuum atmosphere 1.B.4. Controlled 1.B.7. Vacuum or other controlled atmosphere metallurgical melting and casting and melting metallurgical atmosphere controlled other or 1.B.7. Vacuum 1.A.4. in radio be used actions that can to provide Remote manipulators remote

;

3 and 20 000 cm 000 and 20

3 and

or semiconductor wafers. and (1 700 °C); istics: cm 000 1 between capacities electrode 1. Consumable 0,6 m or more (over-the-wall operation). wall operation); °C); (850 123 K 1 above operation of 1. Capable diameter; in less or mm 600 coils 2. Induction kW or more; 3. power Designed inputs for of 5 2B226.a. in specified furnaces designed for 2. Capable of operating with melting temperatures 973 above K 1 b. of bridging A capability wall with a thickness of over the top of a hot cell furnaces and related equipment as follows: character following the of both having furnaces casting and remelt a. Arc Note: 2B226.a. does not control furnaces designed for the processing of processing the for designed furnaces control not does Note: 2B226.a. supplies therefor, as follows: as supplies therefor, 3B. ALSO N.B: SEE characteristics: following the of all having a. Furnaces b. specially kW or more, power output of 5 Power supplies, with a specified chemical separation operations or hot cells, having either of the following the of having either hot cells, or operations separation chemical characteristics: m or more of hot wall (through-the- cell a. A capability of penetrating 0,6 Technical Note: manipulators Remote provide translation of human operator actions to a remote operating arm and They may terminal fixture. be of ‘master/slave’ type or operated by or joystick keypad. 2B227 Vacuum or other controlled atmosphere metallurgical melting and casting and melting metallurgical atmosphere controlled other or 2B227 Vacuum 2B226 Controlled atmosphere (vacuum or inert gas) induction furnaces, and power 2B225 and in radio can be used actions Remote manipulators that to provide remote furnaces, induction gas) inert or (vacuum atmosphere 2B226 Controlled

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 101

machines. (1 200 °C); strength “fibrous or filamentary materials”. strength “fibrous or filamentary furnaces, having both of the following characteristics: following characteristics: having the both of furnaces, and kW or greater; 1. A power of 50 2. Capable of operating with melting temperatures above 473 1 K the furnaces specified in Item 1.B.7.a. or 1.B.7.b. sections, baffles, and end sections, baffles, caps; Note: Item 3.B.2.a. includes precision mandrels, clamps, and shrink fit sections to a common axis; Technical Note: 3.B.2.b. In Item such equipment normally consists of precision measuring subsequently computer that probes linked to a controls the action of, for tube sections. aligning the rotor used rams for example, pneumatic bellows. Technical Note: 3.B.2.c. of the following char to in Item have all The bellows referred acteristics: mm; 400 and 75 between diameter 1. Inside mm; 12,7 than greater or to equal 2. Length and mm; 2 than greater depth convolution 3. Single Made of high-strength aluminium alloys, or high maraging steel, 4. b. Electron b. Electron beam melting furnaces and plasma atomization and melting c. any of for configured specially and monitoring systems Computer control bellows-forming mandrels and dies, as follows: as mandrels and dies, bellows-forming tube rotor gas centrifuge assembly of assembly equipment for Rotor a. tube rotor centrifuge gas of alignment for equipment straightening b. Rotor c. Bellows-forming mandrels and dies for producing single-convolution 3.B.2. Rotor fabrication or assembly equipment, rotor straightening equipment, straightening rotor equipment, assembly or fabrication 3.B.2. Rotor

and

machines. (1 200 °C). strength “fibrous or filamentary materials”. strength “fibrous or filamentary Technical Note: In 2B228.c. the bellows have all of the following characteristics: mm; 400 and mm 75 between diameter 1. Inside mm; 12,7 than greater or to equal 2. Length mm; 2 than greater depth convolution 3. Single sections, baffles, and end sections, baffles, caps; furnaces, having both of the following characteristics: having the following characteristics: both of furnaces, and kW or greater; 1. A power of 50 2. Capable of operating with melting temperatures 473 above K 1 in 2B227.a. specified the furnaces or b. Note: 2B228.a. includes precision mandrels, clamps, and shrink fit sections to a common axis; 4. Made of high-strength aluminium alloys, maraging steel or high Technical Note: In 2B228.b. such equipment normally consists of precision measuring of, action the subsequently controls computer that a to probes linked for example, pneumatic rams used for aligning the rotor tube sections. bellows. bellows-forming mandrels and dies, as follows: as mandrels and dies, bellows-forming tube rotor assembly of gas centrifuge Rotor assembly equipment for a. b. Electron beam melting furnaces and plasma atomization and melting atomization and plasma furnaces beam melting Electron b. of any for configured specially systems monitoring and control c. Computer tube rotor centrifuge gas of alignment for equipment straightening b. Rotor c. Bellows-forming c. Bellows-forming mandrels and dies for producing single-convolution 2B228 Rotor fabrication or assembly equipment, rotor straightening equipment, straightening rotor equipment, assembly or fabrication 2B228 Rotor

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 102 /s; and

of full scale; or of full scale; Pa when measuring at 13 kPa. Technical alloy, aluminium oxide (alumina or sapphire), nickel, nickel alloy with alloy sapphire), nickel, nickel alloy, aluminium oxide or (alumina % nickel by hydrocarbon weight, or fully fluorinated more than 60 polymers; contact with the process medium, by made of or protected direct or sapphire), aluminium, aluminium alloy, oxide (alumina % nickel by weight, or fully fluor nickel, nickel alloy with more than 60 inated hydrocarbon polymers; and % 1. 1 than ± better of than 13 kPa and an “accuracy” of less scale full A 2. A scale of 13 full kPa and or an greater than of better “accuracy” ± 130 into a signal. measurements temperature. ambient at ability gas or air. pump of the blocked off. a. Input throat size equal to or greater than 380 mm; 380 than greater or to equal size throat a. Input m 15 than greater or to equal speed b. Pumping having all of the following characteristics: following the of having all aluminium aluminium, by protected or of made elements sensing a. Pressure b. Seals, if any, for sealing essential the pressure sensing element, and in characteristics: following the of either c. Having Notes: 1. In Item 3.A.7. pressure transducers are devices that convert pressure 2. In Item 3.A.7. “accuracy” includes non-linearity, hysteresis and repeat c. Capable of producing an ultimate vacuum better than 13,3 mPa. 13,3 than better vacuum ultimate an producing of c. Capable Technical Notes: nitrogen with point measurement the at determined is speed pumping 1. The 2. vacuum at the input of the pump determined is The ultimate with the input 3.A.8. Vacuum pumps having all of the following characteristics: following the of all having pumps 3.A.8. Vacuum 3.A.7. All types of pressure transducers capable of measuring absolute pressures and

and /s;

and

or of full-scale; Pa when at 13 measured kPa. 1. % than ± 1 better of than 13 kPa and an ‘accuracy’ of less scale A full gas or air. of the pump blocked off. alloy, aluminum oxide (alumina or sapphire), nickel, nickel alloy with alloy, aluminum or sapphire), oxide (alumina hydrocarbon % nickel by fluorinated weight, or fully than 60 more polymers; contact with the process medium, made of or protected by direct alloy, aluminum oxide or sapphire), aluminium, aluminium (alumina % nickel by weight, or fully fluor nickel, nickel alloy with more than 60 inated hydrocarbon polymers; 2. than ± 130 of better and an ‘accuracy’ of 13 kPa or greater scale A full a signal. measurement into ambient temperature. at and repeatability c. Capable of producing an ultimate vacuum better than 13 mPa. 13 than better vacuum ultimate an producing of c. Capable Technical Notes: nitrogen with point measurement the at determined is speed pumping 1. The 2. The ultimate vacuum is determined at the input of the pump with the input c. Having either of the following characteristics: following the of either c. Having a. Input throat size equal to or greater than 380 mm; 380 than greater or to equal size throat a. Input m 15 than greater or to equal speed b. Pumping Technical Notes: 1. a pressure converts that means a device 2B230 transducer’ ‘pressure In hysteresis non-linearity, includes ‘accuracy’ 2B230, of purposes the 2. For and having all of the following: the of and having all a. sensing elements made of or protected by Pressure aluminium, aluminium in and element, sensing pressure the sealing for essential any, if b. Seals, 2B231 Vacuum pumps having all of the following characteristics: following the of all having pumps 2B231 Vacuum 2B230 capable of measuring absolute pressures transducers’ types All of ‘pressure

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 103

/h or greater;

weapon systems. any of the following materials: following the any of alloy; aluminium or 1. Aluminium oxide; 2. Aluminium steel; 3. Stainless alloy; nickel or 4. Nickel or bronze; 5. Phosphor 6. Fluoropolymers. vanes, or scrolls, spiral intermeshed of trapped between one or more pairs The moving scroll stationary. remains other the which moves while one of orbits the it does stationary scroll; not rotate. As the moving scroll orbits the gas the stationary scroll, pockets diminish in they size (i.e., are compressed) as they move outlet port of the machine. toward the of the pump parts from the lubricated and isolated from the external totally trothermal types, and other advanced systems) capable of accelerating km/s or greater. projectiles to 1,5 high velocity designed for guns specially does not control item Note: This b. and of 2:1 or greater; ratio Capable of a pressure c. come in contact with that the process gas made from surfaces Having all Technical Notes: 1. compressor or vacuum pump, In a scroll pockets of gas are crescent-shaped 2. compressor or vacuum pump, scroll the process gas is In a bellows-sealed pumps having all of the following characteristics: characteristics: following the of pumps having all a. m of 50 volume Capable of an flow rate inlet 5.B.2. High-velocity gun systems (propellant, gas, coil, electromagnetic, and elec and electromagnetic, coil, gas, (propellant, systems gun 5.B.2. High-velocity 3.A.9. Bellows-sealed scroll-type compressors and bellows-sealed scroll-type vacuum scroll-type bellows-sealed and compressors scroll-type 3.A.9. Bellows-sealed

/h or greater;

3 and

or any of the following materials: following materials: the any of alloy; aluminium or 1. Aluminium oxide; 2. Aluminium steel; 3. Stainless alloy; nickel or 4. Nickel bronze; 5. Phosphor 6. Fluoropolymers. b. of 2:1 or greater; a pressure ratio Capable of vacuum pumps having all of the following: the of vacuum pumps having all 2B350.i. ALSO N.B.: SEE m 50 of rate flow volume inlet an of a. Capable c. with the process gas made from come in contact that surfaces Having all trothermal types, and other advanced systems) capable of accelerating km/s or greater. projectiles to 1,5 CONTROLS. GOODS MILTARY ALSO N.B.: SEE 2B233 Bellows-sealed scroll-type compressors and bellows-sealed scroll-type bellows-sealed and compressors scroll-type 2B233 Bellows-sealed 2B232 High-velocity gun systems (propellant, gas, coil, electromagnetic, and elec and electromagnetic, coil, gas, (propellant, systems gun 2B232 High-velocity

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 104

1.B.3.d. includes “software” for simultaneous measurements of wall of measurements simultaneous for “software” 1.B.3.d. includes thickness and contour. horities of the Member State in which they are established. atmosphere by bellows. One a metal end of the bellows is attached to the housing the of stationary the to attached end is other and the moving scroll pump. Polytetrafluoroethylene (PTFE), b. Fluorinated Ethylene Propylene (FEP), and (PCTFE); e. d. c. Perfluoroalkoxy (PFA), Polychlorotrifluoroethylene copolymer. Vinylidene fluoride-hexafluoropropylene 3. Fluoropolymers include, but are not limited to, the following materials: a. materials: following the to, limited not are but include, 3. Fluoropolymers specified in Item 1.A.3., 1.B.1., 1.B.3., 1.B.5., 1.B.6.a., 1.B.6.b., 1.B.6.d. or 1.B.7. Item in specified systems for modified or designed specially Note: “Software” device(s) to function as a “numerical control” unit for machine tools, that is control” unit for to function as a “numerical device(s) axes that can be coordinated capable of controlling five or more interpolating “contouring control”. simultaneously for Nuclear Suppliers Group's as in control list INFCIRC/254/Rev.9/Part2 1.D.2. designed specially “use” of equipment or modified for the “Software” 1.D.3. “Software” for any combination of electronic devices or system enabling such enabling system or devices electronic of combination any for 1.D.3. “Software”

transit of dual-use items “numerical control” codes for machining codes for “numerical control” various parts. duction”in 2A001 of equipment specified or 2B001 2B009. 2B003 to 2B001 or 2A001.c., in specified Note: 2D001 does not control part programming “software” that generates that “software” programming part control not does Note: 2D001 or system, enabling such devices or systems to function as a “numerical than four axes co-ordinating simultaneously more unit, capable of control” for “contouring control”. a. specially designed or modified for the “development” “Software” or “pro of equipment designed the “use” or modified for specially “Software” b.

2D002 “Software” for electronic devices, even when residing in an electronic device 2D001 “Software”, other than that specified in 2D002, as follows: as 2D002, in specified that than other 2D001 “Software”, ) 230/2 calculating positioning accordance with ISO Manufacturers accuracy in (1997) or (2006) should consult competent aut the

2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and brokering exports, transfer, of control the for 5 Community 2009 of regime a up May 2009 setting 1 The corresponding Council No 428/ in systems, equipment Regulation (EC) and components identified as 2D Software ( M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 105

1.B.3.d. includes “software” for simultaneous measurements of wall of measurements simultaneous for “software” 1.B.3.d. includes thickness and contour. wall of measurements simultaneous for “software” 1.B.3.d. includes thickness and contour. generates “numerical control” generates “numerical control” command codes but does not allow direct use of equipment for machining various parts. “numerical control” control” unit “numerical or any device or system. electronic of the control unit or machine tool to the manufacturers operate a machine 1.B.2. in Item is not specified tool that Notes: 1. “Software” is controlled whether exported separately or residing in a by modified or designed specially “software” control not does 1.D.3. 2. Item specified in Item 1.A.3., 1.B.1., 1.B.3., 1.B.5., 1.B.6.a., 1.B.6.b., 1.B.6.d. or 1.B.7. Item in specified systems for modified or designed specially Note: “Software” specified in Item 1.A.3., 1.B.1., 1.B.3., 1.B.5., 1.B.6.a., 1.B.6.b., 1.B.6.d. or 1.B.7. Item in specified systems for modified or designed specially Note: “Software” tion”, or “use” of equipment specified in Item 1.B.2. tion”, in Item or “use” of equipment specified Note: Item 1.D.2. does not control part programming “software” that 1.D.1. designed specially “use” of equipment or modified for the “Software” 1.D.1. designed specially “use” of equipment or modified for the “Software” 1.D.2. “Software” specially designed or modified for the “development”, “produc “development”, the for modified or designed specially 1.D.2. “Software”

minimum necessary for the operation of, items not specified by Category 2. the operation of items not specified in not the operation Category of items specified 2. 2B002. in specified items for “software” 2D003 for 2D001 and “numerical control” command codes but does not allow direct use of use command “numerical control” but does not allow direct codes machining equipment for various parts. Note 3: 2D002 does not control “software” that is exported with, and the 2B206, 2B207, 2B209, 2B219 or 2B227. or 2B207, 2B209, 2B219 2B206, in 2B201. duction” of equipment or “use” specified specified in 2B104, 2B105, 2B109, 2B116, 2B117 or 2B119 to 2B122. to 2B119 or 2B105, 2B109, 2B116, 2B117 2B104, in specified 9D004. ALSO N.B.: SEE Note 1: 2D002 does not control “software” specially designed or modified for modified or designed specially “software” control Note 1: not does 2D002 Note 2: 2D002 does not control “software” for items specified in 2B002. See Note: 2D202 does not control part programming “software” that generates that “software” programming part control not does Note: 2D202 2D201 “Software” specially designed for the “use” of equipment specified in 2B204, in specified equipment of “use” the for designed specially “pro 2D201 “Software” “development”, the for modified or designed specially 2D202 “Software” 2D101 “Software” specially designed or modified for the “use” of equipment of “use” the for modified or designed specially 2D101 “Software”

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 106

“production” or “use” of equipment, material or “software” specified in 1.A. specified or “software” “production” or “use” of equipment, material through 1.D. in 1.A. specified or “software” “production” or “use” of equipment, material through 1.D. in 1.A. specified or “software” “production” or “use” of equipment, material through 1.D. “production” or “use” of equipment, material or “software” specified in 1.A. specified or “software” “production” or “use” of equipment, material through 1.D. Nuclear Suppliers Group's as in control list INFCIRC/254/Rev.9/Part2 1.E.1 “Technology” according to the Technology Controls for the “development”, 1.E.1 “Technology” according to the Technology Controls for the “development”, 1.E.1 “Technology” according to the Technology Controls for the “development”, 1.E.1 “Technology” according to the Technology Controls for the “development”,

transit of dual-use items coordinate measurement machines specified in 2B006.a. coordinate measurement machines specified opment” of equipment or “software” specified in 2A, opment” specified 2B of equipment or 2D. or “software” duction”in 2A of equipment specified or 2B 2B004, 2B009, 2B104, 2B109, 2B116, in specified “software” or equipment 2D101. 2B122 or 2B119 to 2A225, 2A226, 2B001, 2B006, in specified “software” or equipment 2B007.b.,2B007.c., 2B008, 2B009, 2B201, 2B204, 2B206, 2B207, 2B209, 2D202. 2B233, 2D201 or 2B225 to Note: 2E001 includes “technology” for the integration of probe systems into systems probe of integration the for “technology” includes Note: 2E001

2E001 “Technology” according to the General Technology Note for the “devel the for Note Technology General the to according 2E001 “Technology” 2E002 “Technology” according to the General Technology Note for the “pro the for Note of Technology “use” General the the for to according Note 2E002 “Technology” Technology of General “use” the the to for according Note 2E101 “Technology” Technology General the to according 2E201 “Technology” 2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and brokering exports, transfer, of control the for 5 Community 2009 of regime a up May 2009 setting The corresponding Council No 428/ in systems, equipment Regulation (EC) and components identified as 2E Technology M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 107

relationship.

F; and F; and as part of μ μ medical nuclear magnetic resonance (NMR) nuclear medical does not necessarily mean physical part in the same the in physical part mean does not necessarily as part of exported imaging systems. shipment. As part of, volume. 2. Energy storage greater than 10 J; 2. than 10 Energy storage greater 0,5 than greater 3. Capacitance or nH; 50 than less inductance 4. Series 0,25 than greater 2. Capacitance 3. Series inductance less than 10 nH. 10 than less inductance 3. Series

acteristics: acteristics: T; 2 than greater fields magnetic creating of a. Capable 2; than greater diameter inner to length of ratio b. A and mm; 300 than greater diameter c. Inner d. % of the inner 50 % over the central than 1 uniform to better Magnetic field Note: Item 3.A.4. does not control magnets specially designed for and N.B.: istics: kV; 1,4 than greater rating Voltage a. 1. V; 750 than greater rating b. 1. Voltage Separate shipments from sources different are allowed, provided the related specify the export documents clearly Nuclear Suppliers Group's as in control list INFCIRC/254/Rev.9/Part2 3.A.4. Superconducting solenoidal electromagnets having all of the following char following the of all having electromagnets solenoidal 3.A.4. Superconducting 6.A.4. Pulse discharge capacitors having either of the following sets of character of sets following the of either having capacitors discharge 6.A.4. Pulse CATEGORY 3 — ELECTRONICS — CATEGORY 3

or and and and F; F; μ μ

transit of dual-use items exported ‘as parts of’ medical nuclear magnetic resonance medical nuclear magnetic exported ‘as parts of’ (NMR) imaging systems. The phrase ‘as part of’ does not necessarily mean physical part in the same shipment; separate allowed, provided the sources are different shipments from related export documents clearly specify that the shipments are imaging systems. the part of’ dispatched ‘as inner volume; d. Series inductance less than 50 nH; 50 than less inductance d. Series b. Capacitance greater than 0,25 than greater b. Capacitance c. Series inductance less than 10 nH; 10 than less inductance c. Series b. Energy storage greater than 10 J; 10 than greater storage b. Energy 0,5 than greater c. Capacitance Note: 3A201.b. does not control magnets specially designed for and characteristics: characteristics: T; 2 than greater fields magnetic creating of 1. Capable 2; than greater diameter inner to length of ratio 2. A mm; 300 than greater diameter 3. Inner 4. Magnetic field uniform to better than 1 % over the central 50 % of the 4. 50 % over the central than 1 uniform to better Magnetic field 2. a. Voltage rating greater than 750 V; 750 than greater rating 2. a. Voltage 1. a. Voltage rating greater than 1,4 kV; 1,4 than greater rating 1. a. Voltage a. having Capacitors of the following sets characteristics: either 3A201 b. Superconducting solenoidal electromagnets having all of the following the of all having electromagnets solenoidal Superconducting 3A201 b. 3A201 Electronic components, other than those specified in 3A001, as follows; as 3A001, in specified those than other components, 3A201 Electronic 2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and brokering exports, transfer, of control the for 5 Community 2009 of regime a up May 2009 setting The corresponding Council No 428/ in systems, equipment Regulation (EC) and components identified as Components and Equipment 3A Systems, M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 108 s. Q equals μ Q. V is the peak the Q. V is

2,65 V

3 s, then Q is the total accelerated accelerated the total s, then Q is μ idt ) where i is beam current in current is beam i where ) idt ∫

25 MeV; and devices designed for purposes other than electron beam or X-ray microscopy, radiation (electron for example) nor those designed for medical purposes. electron energy in million electron volts. If the beam accelerator pulse than less or equal to 1 duration is charge in Coulombs. beam pulse duration the is greater accelerator If charge in 1 ms, then the maximum accelerated Q is than 1 2. or (K) of 0,25 merit or greater; a figure of With MW. 50 than greater power peak 2. A the integral of i with respect to t, over the lesser of 1 ms or the time of 1 of i with respect to t, over the the integral lesser duration of the beam pulse = (Q amperes and in seconds. t is the time ms or the duration of bunched beam the beam pulse of 1 is the lesser packet resulting from one microwave modulator pulse. a bunched duration of the time beam in current is the average current packet. following sets of characteristics: a. 1. peak energy electron of 500 An accelerator but keV less than or greater b. 1. and energy peak of 25 electron MeV or greater; An accelerator Note: Item 5.B.1. does not control accelerators that are component parts of Technical Notes: × 10 1. K = 1,7 defined as: K is of merit The figure 2. amperes). in beam current × (peak volts) in potential Peak power = (peak of duration time the cavities, accelerating microwave on based machines 3. In 4. In machines based on microwave accelerating cavities, the peak beam 5.B.1. having of the either or pulsed accelerators Flash X-ray generators electron s, μ s or μ and or idt), where i is beam idt), ∫ s, then Q is the maximum s, then Q is μ

s. μ

and 2,65 V

devices designed for purposes other than electron beam or X-ray designed for nor those example) for microscopy, radiation (electron medical purposes: than 25 MeV; K = 1,7 × 10 K = 1,7 b. A ‘peak power’ greater than 50 MW. b. than A 50 ‘peak power’ greater b. of 0,25 (K) or greater; of merit’ With a ‘figure V is the peak electron energy in million electron volts. energy in million electron V is the peak electron If the accelerator beam pulse duration is less than or equal to 1 then Q charge is the total accelerated in Coulombs. the accelerator If than 1 greater duration is beam pulse accelerated charge in 1 of 1 the lesser over to t, Q equals of i with respect the integral duration the time of the beam = pulse (Q current in amperes and in seconds. t is time amperes). following sets of characteristics: of following sets 1. a. peak energy electron An of 500 accelerator but keV less or greater Technical Notes: 1. defined as: K is The ‘figure of merit’ Note: 3A201.c. does not control accelerators that are component parts of parts component are that accelerators control not does Note: 3A201.c. 2. a. energy peak of 25 electron MeV An or greater; accelerator 2. ‘Peak power’ = (peak potential in volts) × (peak beam × (peak current in ‘Peak power’(peak potential in volts) = 2. 3A201 c. of the having either accelerators or pulsed electron generators Flash X-ray

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 109

for the gas process centrifuge are controlled under INFCIRC/254/Part amended). 1 (as below the characteristics meet to of frequency changers or generators is controlled in 3.D.2 and 3.D.3. industrial machinery and/or consumer goods (machine tools, vehicles, above if the frequency when changers can etc.) meet the characteristics Note 3. removed, and subject to General above, taking the characteristics frequency changer meets or not a particular constraints. and into account hardware software N.B.1: Frequency changers and generators especially designed or prepared or frequency motor drive, having all of the following characteristics: designed especially generators and changers N.B.1: Frequency performance the release or enhance to designed specially N.B.2: “Software” a. greater; VA or 40 of power output providing a Multiphase and Hz or more; b. at a frequency of 600 Operating %. 0,2 than (less) better control c. Frequency Notes: 1. Item 3.A.1. only controls frequency changers intended for specific 2. whether For the purpose determine of export control, the Government will 3.A.1. Frequency frequency or fixed changers or generators, usable as a variable

or s or the duration of the μ

and

enhancements or release the constraints; the release enhancements or the performance release of 3A225; to meet the characteristics performance of a frequency changer or generator to meet the char the meet changer generator to or a frequency performance of of 3A225 in 3D225. is specified acteristics performance of a frequency changer or generator to meet the char the meet changer generator to or a frequency performance of of 3A225 in 3E225. is specified acteristics hardware, “software” or “technology”the constraints that limit meet above, provided they specified than that less performance to following: the any of 1. They need to be returned the original manufacturer to make the in 3D225 They require “software” as specified to enhance or 2. duration of the beam of 1 pulse is the lesser modulator microwave pulse. one from resulting bunched beam packet current is the average current in the time duration of a bunched beam packet. 3. In machines based on microwave accelerating cavities, the time the cavities, machines based on microwave accelerating 3. In 4. beam peak the cavities, on microwave accelerating machines based In Note: 3A225 does not control frequency changers or generators if they have they if generators or changers frequency control not does Note: 3A225 N.B. 1: “Software” specially designed to enhance or release the N.B. 2: the to enhance “Technology”or release form of codes or keys in the usable as a variable or fixed frequency motor drive, having all of the frequency motor drive, having of or fixed all variable usable as a following characteristics: c. Frequency control better (less) than 0,2 %. 0,2 than (less) better control c. Frequency a. Multiphase output providing a power of 40 VA or greater; Hz or more; b. Operating at a frequency of 600 3A225 Frequency changers or generators, other than those specified in 0B001.b.13., in specified those than other generators, or changers 3A225 Frequency

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 110

ariable Speed Drives

ariable Speed Motor Drives, V ariable Frequency Drives (VFDs), Adjustable Frequency Drives inverters. Equipment, AC equipment marketed such Test as: Generators, Electronic Power Supplies, V (VSDs), V (AFDs), or Adjustable Speed Drives (ASDs). greater with current output of 1 A or greater; and A or greater; output of 1 with current greater greater with current output of 500 A or greater; and A or greater; output of 500 with current greater gap, having all of the following characteristics: following the of gap, having all electrodes; more or three 1. Containing kV or more; 2. Anode of 2,5 peak voltage rating Technical Notes: Technical 1. Frequency changers in Item 3.A.1. are also known as converters or 2. The characteristics specified in item 3.A.1. may be met by certain acteristics: acteristics: a. kV or Capable of continuously producing, period of 8 hours, 20 over a time b. period of 8 hours. % over a time than 0,1 better or voltage stability Current acteristics: acteristics: a. V or Capable of continuously producing, period of 8 hours, 100 over a time b. period of 8 hours. % over a time than 0,1 better or voltage stability Current a. Cold-cathode tubes, whether gas filled or not, operating similarly to a spark a to similarly operating not, or filled gas whether tubes, a. Cold-cathode 3.A.6. High-voltage direct current power supplies having both of the following char following the of both having supplies power current direct 3.A.6. High-voltage 3.A.5. following char the having both of power supplies current High-power direct 6.A.3. Switching devices as follows: as devices 6.A.3. Switching

and and

in 3E225 to enhance or the performance release to meet the char of 3A225. acteristics 3. or codes as specified form of keys They require “technology” in the hours. hours. Test Equipment, AC Power Supplies, Variable Speed Motors Drives, Variable Speed (VSDs), Variable Drives Frequency (VFDs), or Adjustable Speed Drives (ASDs). Adjustable Frequency Drives (AFDs), A or greater; output of 1 with current or greater spark gap, having of the following characteristics: all electrodes; more or three 1. Containing kV or more; 2. Anode of 2,5 peak voltage rating or greater with current output of 500 A or greater; output of 500 with current or greater b. Current or voltage stability better than 0,1 % over a time period of 8 than 0,1 better b. Current or voltage stability b. Current or voltage stability better than 0,1 % over a time period of 8 than 0,1 better b. Current or voltage stability Technical Notes: 1. Frequency changers in 3A225 are also known as converters or inverters. Electronic Generators, as marketed be may 3A225 in changers 2. Frequency 0B001.j.5., having the following characteristics: both of a. kV Capable of continuously producing, period over a of 8 time hours, 20 a to similarly operating not, or filled gas whether tubes, a. Cold-cathode 0B001.j.6., having the following characteristics: both of a. V Capable of continuously producing, period over a of 8 time hours, 100 3A227 High-voltage direct current power supplies, other than those specified in specified those than other supplies, power current direct 3A227 High-voltage follows: as devices, 3A228 Switching 3A226 High-power direct current power supplies, other than those specified in specified those than other supplies, power current direct 3A226 High-power

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 111 s into loads of less loads of s into μ

s or less; and s or less; s or less; μ μ s or less. μ than 40 ohms; 2. Rated for a peak current of 500 A or more; 2. of 500 Rated for a peak current following characteristics: kV; 2 than greater rating voltage peak 1. Anode and more; or A 500 of rating current peak 2. Anode 1 of time 3. Turn-on Note: Item 6.A.3.a. includes gas krytron tubes and vacuum sprytron tubes. 15 of time delay 1. Anode 3. Anode peak current rating of 100 A or more; and A or more; 3. Anode rating of 100 peak current 10 of time delay 4. Anode charged, explosively-driven and optically-driven firing sets designed to sets firing charged, explosively-driven and optically-driven drive multiple controlled detonators specified by Item 6.A.1. above; characteristics: ruggedized-use; or mobile, portable, for 1. Designed 15 than less in energy their delivering of 2. Capable 3. Having an output greater than 100 A; 100 than greater output an 3. Having cm; 30 than greater dimension 4. No and kg; 30 than less 5. Weight c. switching function having Modules with a fast of the all or assemblies b. Triggered spark-gaps having both of the following characteristics: following the of both having spark-gaps b. Triggered a. Detonator firing sets (initiation systems, firesets), including electronically- including firesets), systems, (initiation sets firing a. Detonator following the of having all (pulsers) pulse generators electrical b. Modular 6.A.2. as follows: pulse generators, and equivalent high-current sets Firing

s into loads of less

μ and and and

s or less; μ s or less; μ s or less. μ than 40 ohms; Note: 3A228 includes gas krytron tubes and vacuum sprytron tubes. 15 of time delay anode 1. An than other sets, firing and optically-driven charged, explosively-driven in 1A007.a., those specified designed controlled to drive multiple in 1A007.b.; detonators specified characteristics: ruggedized-use; or mobile, portable, for 1. Designed 15 than less in energy their delivering of 2. Capable A; 100 than greater output an 3. Having cm; 30 than greater dimension 4. No 4. Anode delay time of 10 of time delay 4. Anode 1 of time 3. Turn-on 3. Anode peak current rating of 100 A or more; 3. Anode rating of 100 peak current 2. Rated for a peak current of 500 A or more; 2. of 500 a peak current Rated for in 3A001.g. specified or 3A001.h., having of the following character all istics: kV; 2 than greater rating voltage peak 1. Anode A or more; 2. Anode rating of 500 peak current N.B.: SEE ALSO MILITARY GOODS CONTROLS. GOODS MILITARY ALSO N.B.: SEE electronically- including firesets), systems, (initiator sets firing a. Detonator following the of all having (pulsers) generators pulse electrical b. Modular b. Triggered spark-gaps having both of the following characteristics: characteristics: following the of both having spark-gaps b. Triggered c. Modules or assemblies with a fast switching function, other than those than other function, switching fast a with assemblies or c. Modules 3A229 High-current pulse generators as follows: as generators pulse 3A229 High-current

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 112

(–50 °C to 100 °C) or specified as suitable for aerospace applications. aerospace for as suitable °C) or specified °C to 100 (–50 include both explosive sets charging. Explosively-driven firing and laser and explosive ferroelectric firing set ferromagnetic types. Item 6.A.2.b. includes xenon drivers. flashlamp and between 10 % and 90 % voltage amplitude. can include of pulse that forms function and shape into a variety it step, impulse, exponential, monocycle or types. triangular, rectangular, they can be a the pulse generator, of part Pulse heads can be an integral connected device. be an externally or they can device plug-in module to the 6. of 223 373 range to K an extended temperature over operate to Specified mm; 35 than greater dimension 1. No and kV; 1 than greater or to equal of rating 2. Voltage nF. 100 than greater or to equal of 3. Capacitance following characteristics: a. than 55 load of less ohms; V into a resistive than 6 Output voltage greater ps. 500 than less time’ transition b. ‘Pulse Technical Notes: 1. In Item 5.B.6.b. ‘pulse transition time’ is defined as the time interval step voltage a accept to designed networks forming impulse are heads 2. Pulse c. Micro-firing units having all of the following characteristics: following the of all having units c. Micro-firing Note: Optically driven firing sets include both those employing laser initiation 5.B.6. the having both of heads therefor, and pulse pulse generators, High-speed

and

to 373 K (100 °C) or specified as suitable for aerospace applications. for as suitable °C) or specified to 373 K (100 10 % and 90 % voltage amplitude. step function and of pulse forms that can shape into a include variety it types. monocycle exponential, or impulse, rectangular, triangular, step, heads’ can be an integral part the pulse generator, can be of ‘Pulse they a plug-in module or they can to the device be connected an externally device. 5. Weight less than 30 kg; 30 than less 5. Weight Note: 3A229.b. includes xenon flash-lamp drivers. mm; 35 than greater dimension 1. No kV; 2. than 1 Voltage rating of equal to or greater 6. Specified for use over an extended temperature range 223 K (–50 °C) 6. 223 range (–50 K an extended temperature use over for Specified 3. than 100 Capacitance of equal to or greater nF. and following characteristics: a. than 55 less ohms, load of V into a resistive than 6 Output voltage greater Technical Notes: between interval time the as defined is time’ transition ‘pulse 3A230, 1. In voltage a accept to designed networks forming impulse are heads’ 2. ‘Pulse c. Micro-firing units having all of the following characteristics: following the of all having units c. Micro-firing b. ‘Pulse transition time’ less than 500 ps. 500 than less time’ transition b. ‘Pulse 3A230 having both of the therefor, heads’and ‘pulse High-speed pulse generators,

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 113

2 neutrons/s or

9 s. μ

such as lead azide. lead such as reaction; or reaction; × 10 and capable nuclear reaction of an output of 3 greater. 1. Exploding bridge (EB); bridge 1. Exploding (EBW); wire bridge 2. Exploding 3. Slapper; (EFI); initiators foil 4. Exploding (see 3A232) mm 000 than 5 greater area an over an explosive surface taneously initiate 2. Utilizing electrostatic acceleration to induce a deuterium-deuterium from a single firing signal with timing spread over from a single firing an initiation the surface than 2,5 of less a. Electrically driven explosive detonators, as follows: as detonators, explosive driven a. Electrically simul nearly to designed detonators multiple or single using b. Arrangements characteristics: characteristics: and system; vacuum external an without operation for a. Designed nuclear tritium-deuterium a induce to acceleration electrostatic b. 1. Utilizing Note: Item 6.A.1. does not control detonators using only primary explosives, primary only using detonators control not does 6.A.1. Note: Item Technical Note: conductor electrical a small 6.A.1. In Item utilize the detonators of concern all (bridge, bridge wire, or that explosively foil) vaporizes when a fast, high- pulse is passed through In nonslapper types, it. the electrical current highexplosive contacting a in detonation chemical a starts exploding conductor 6.A.1. Detonators and multipoint initiation systems, as follows: as systems, initiation multipoint and 6.A.1. Detonators 6.A.5. Neutron generator systems, including tubes, having both of the following the of both having tubes, including systems, generator 6.A.5. Neutron

2 and

neutrons/s or greater.

μ or as lead azide. reaction; reaction and capable of an output of 3 × 10 and capable of an output reaction of 3 1. Electrostatic 1. Electrostatic acceleration to induce a tritium-deuterium nuclear 2. Electrostatic 2. Electrostatic acceleration to induce a deuterium-deuterium nuclear simultaneously initiate an explosive surface over greater than 5 000 mm 000 than 5 over greater an explosive surface simultaneously initiate from a single firing signal with an initiation over timing spread the surface signal with an initiation a single firing from than 2,5 of less b. Utilizing any of the following: the of any b. Utilizing Note: 3A232 does not control detonators using only primary explosives, such explosives, primary only using detonators control not does Note: 3A232 characteristics: system; vacuum external an without operation for a. Designed detonators. for 1A007.b. N.B.: See used; a. Not b. Arrangements using single or multiple detonators designed to nearly N.B.: SEE ALSO MILITARY GOODS CONTROLS. GOODS MILITARY ALSO N.B.: SEE 3A231 systems, including tubes, having following the both of Neutron generator 3A232 Multipoint initiation systems, other than those specified in 1A007, as follows: as 1A007, in specified those than other systems, initiation 3A232 Multipoint

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 114 . In slapper detonators, the slapper . In

line samples of uranium hexafluoride are controlled under INFCIRC/ amended). 254/Part 1 (as molecules into a region of the ion source where the molecules are the molecules into a region of the ion source where molecules ionized by an beam; and electron not that are ionized °C) or less in order to trap analyte molecules (–80 beam; electron by the features: 1. beam of analyte a collimated injects system that beam inlet A molecular K 193 of temperature a to cooled be can that traps cold more or 2. One for actinides or actinide fluorides. greater and having than 2 greater in 230, parts a resolution of better as follows, and therefor: ion sources on- analyzing for prepared or designed especially spectrometers N.B.: Mass (ICP/MS); spectrometers mass plasma coupled a. Inductively (GDMS); spectrometers mass discharge b. Glow (TIMS); spectrometers mass ionization c. Thermal having both the following bombardment of spectrometers mass d. Electron designed source ion microfluorination a with equipped spectrometers e. Mass material such as PETN (pentaerythritoltetranitrate) conductor or slapper drives a flyer explosive vaporization of the electrical a of the slapper on a gap, and an explosive the impact across starts chemical detonation. The slapper in some designs is driven by magnetic a EB or an to either may refer detonator exploding foil term The force. slapper-type detonator. Also, the word is sometimes used initiator in place word of the detonator. 3.B.6. Mass spectrometers capable of measuring ions of 230 atomic mass units or units mass atomic 230 of ions measuring of capable spectrometers 3.B.6. Mass and

analyte molecules into a region of the ion source where the ionized molecules are by an beam; electron (–80 °C); (–80 electron impact mass spectrometers or electron ionization mass spectro meters. purposes of For the them on cold surfaces. condensing or freezing 3A233.d.2., a closed-loop gaseous helium cryogenic vacuum pump is not a ‘cold trap’. features: 1. A molecular beam inlet system that injects a collimated beam of 2. that can be of 193 One cooled or more ‘cold traps’ to a K temperature for actinides or actinide fluorides. Technical Notes: as known also are 3A233.d. in spectrometers mass bombardment 1. Electron 2. In 3A233.d.2., a ‘cold trap’ is a device that traps gas molecules by measuring ions of 230 atomic mass units or greater and having measuring ions of 230 mass units or greater a resolution atomic in 230, than 2 parts as follows, and of better ion sources therefor: (ICP/MS); spectrometers mass plasma coupled a. Inductively (GDMS); spectrometers mass discharge b. Glow (TIMS); spectrometers mass ionization c. Thermal following the of both having spectrometers mass bombardment d. Electron f. Mass spectrometers equipped with a microfluorination ion source designed source ion used; microfluorination e. Not a with equipped spectrometers f. Mass 3A233 Mass spectrometers, other than those specified in 0B002.g., capable of capable 0B002.g., in specified those than other spectrometers, 3A233 Mass

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 115

“production” or “use” of equipment, material or “software” specified in 3.A. specified or “software” “production” or “use” of equipment, material through 3.D. characteristics: characteristics: and kV; 2 than greater rating a. Voltage nH. 20 than less of b. Inductance acteristics of equipment controlled in Item 3.A.1. of equipment in Item controlled acteristics 3.A.1., 3.B.3. or 3.B.4. 3.A.1., 3.B.3. or Nuclear Suppliers Group's as in control list INFCIRC/254/Rev.9/Part2 Nuclear Suppliers Group's as in control list INFCIRC/254/Rev.9/Part2 3.E.1 “Technology” according to the Technology Controls for the “development”, 6.A.6. the following to provide low inductance path detonators with Striplines 3.D.3. “Software” specially designed to enhance or release the performance char performance the release or enhance to designed specially 3.D.3. “Software” 3.D.1. designed in specially for the “use” of equipment Items specified “Software”

and m; μ and transit of dual-use items transit of dual-use items

layers. b. Incorporating multi-layer structures with three or fewer metal equipment or components controlled by 3A003. components by equipment or controlled “production”specified in 3A001.a.3. of integrated circuits to following: the of all 3A001.a.12., having 0,130 above or at “technology” a. Using

Note 1: 3E001 does not control “technology” for the “production” of b Inductance of less than 20 nH. 20 than less of b Inductance opment” or “production” of specified in equipment 3A, or materials 3B or 3C; frequency changers or generators to meet the characteristics of 3A225. the characteristics to meet frequency changers or generators characteristics: kV; 2 than greater rating a. Voltage Note 2: 3E001 does not control “technology” for the “development” or 2: Note 3B001.a. to f., 3B002 or 3A225

3E001 “Technology” according to the General Technology Note for the “devel the for Note Technology General the to according 3E001 “Technology” 3D225 “Software” specially designed to enhance or release the performance of performance the release or enhance to designed specially 3D225 “Software” 3A234 to provide low inductance path to detonators with the following Striplines 3D002 in equipment of specified the “use” designed for specially “Software” 2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and brokering exports, transfer, of control the for 5 Community 2009 of regime a up May 2009 setting 2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and brokering exports, transfer, of control the for 5 Community 2009 of regime a up May 2009 setting The corresponding Council No 428/ in systems, equipment Regulation (EC) and components identified as The corresponding Council No 428/ in systems, equipment Regulation (EC) and components identified as 3D Software 3E Technology M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 116

Nuclear Suppliers Group's as in control list INFCIRC/254/Rev.9/Part 2 “production” or “use” of equipment, material or “software” specified in 3.A. specified or “software” “production” or “use” of equipment, material through 3.D. “production” or “use” of equipment, material or “software” specified in 3.A. specified or “software” “production” or “use” of equipment, material through 3.D. 3.A.2 N. B. also in correspondence See to 6A205 3.E.1 “Technology” according to the Technology Controls for the “development”, 3.E.1 “Technology” according to the Technology Controls for the “development”,

, and ‘non-repetitive pulsed’ , and ‘non-repetitive 2

CATEGORY 6 — SENSORS AND LASERS AND SENSORS — CATEGORY 6

items

length change) by means other than one “laser” pumping another “laser” is determined by applying the control parameters for both the output of the output. optical frequency-converted and the source “laser” Nd:glass “lasers” are only specified in 6A005.d. in only specified are Nd:glass “lasers” pulses superimposed. Note 1: include those that run in a Pulsed “lasers” continuous mode with wave (CW) Note 2: Excimer, semiconductor, chemical, CO, CO performance of frequency changers or generators to meet the characteristics to meet the characteristics of frequency changers or generators performance of 3A225. wave (i.e., conversion frequency incorporating “lasers” of status Note 4: control The equipment specified in 3A001.e.2., in equipment specified 3A001.e.3., 3A001.g., 3A201, 3A225 to 3A234. optical equipment, as follows: 6A205. ALSO N.B.: SEE Note 3: 6A005 “lasers”. fibre includes Technical Note: ‘Non-repetitive pulsed’ refers to “lasers” that produce either a single output pulse or between pulses exceeding one minute. interval that have a time 3E225 the release codes or keys, to enhance “Technology”,or form of in the 3E201 “Technology” according to the General Technology Note for the “use” of “use” the for Note Technology General the to according 3E201 “Technology” 6A005 “Lasers”, other than those specified in 0B001.g.5. or 0B001.h.6., components and components 0B001.h.6., or 0B001.g.5. in specified those than other 6A005 “Lasers”, The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/2009 of Council Regulation (EC) in identified corresponding equipment and components as systems, The 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual-use of 5 brokering and transit exports, transfer, control of the Community May 2009 for up a regime setting Components and Equipment 6A Systems, M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 117

or or

to or less than to or less 50 W. a. Ruby with output energy below 20 J; 20 below energy output with a. Ruby b. Nitrogen; c. Krypton. b. mode output and power exceeding 150 W; transverse Multiple power exceeding 30 W; W; following: 50 exceeding power output and output mode transverse a. Single b. mode output and power exceeding 80 W; transverse Multiple Note: 6A005.a.2. does not control Argon “lasers” having an output power equal power output an having “lasers” Argon control not does Note: 6A005.a.2. W; following: 50 exceeding power output and output mode transverse a. Single power exceeding 30 W; 4. Output wavelength exceeding 540 nm but not exceeding 800 nm and output nm but not exceeding 800 4. Output wavelength exceeding 540 5. nm and any of the nm but not exceeding 975 Output wavelength exceeding 800 3. nm and any of the nm but not exceeding 540 Output wavelength exceeding 510 1. Output wavelength less than 150 nm and output power exceeding 1 W; W; 1 exceeding power output and nm 150 than less wavelength 1. Output nm and output nm or more but not exceeding 510 2. Output wavelength of 150 Note 5: 6A005 does as follows: not control “lasers” Technical Note: is defined as the ratio of “laser” output power In 6A005 (or efficiency’ ‘Wall-plug “average input power output required power”)to operate to total electrical the “laser”, power supply/conditioning conditioning/heat exchanger. and including the thermal a. Non-“tunable” continuous having lasers” any wave “(CW) of the following:

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 118

;

2 or

and having all of the following: the of having all mrad; • 1. Beam Parameter mm Product (BPP) exceeding 0,7 2. ‘Brightness’ not exceeding 1 024 W/( mm • mrad) • mm W/( 024 1 exceeding not 2. ‘Brightness’ having a BPP exceeding 1,25 mm • mrad • mm 1,25 exceeding BPP having a mrad; • mm 1,7 exceeding BPP having a mrad; • mm 2,5 exceeding BPP having a “lasers” with output power exceeding 2 kW and not exceeding 6 kW and with output kW “lasers” not exceeding 6 power exceeding 2 mass than with a total greater 1 200 kg. For the purpose of this note, total mass includes all components required to operate the “laser”, external excludes exchanger, but power supply, heat e.g., “laser”, optics for beam conditioning and/or delivery. “lasers” having “lasers” any of the following: and kW Output power exceeding 500 a. W but not exceeding 1 b. Output power exceeding 1 kW but not exceeding 1,6 kW and kW but not exceeding 1,6 Output b. power exceeding 1 kW and c. kW but not exceeding 2,5 Output power exceeding 1,6 kW and kW but not exceeding 3,3 d. Output power exceeding 2,5 all-plug efficiency’ exceeding 18 % and output % power exceeding 500 exceeding 18 efficiency’ all-plug or W; Note 1: 6A005.a.6.b. does not control multiple transverse mode, industrial 1. ‘W 1. ‘W kW; 2 exceeding power 2. Output Note 2: 6A005.a.6.b. does not control multiple transverse mode, industrial b. Multiple transverse mode output and any of the following: the of any and output mode transverse b. Multiple following: W; 200 exceeding power output and mode transverse a. Single 6. 150 Output wavelength exceeding 975 nm and any of the nm but not exceeding 1

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 119

1. Operating at wavelengths between 500 and 600 nm; and nm; 600 and 500 between wavelengths at 1. Operating W; 30 than greater or to equal power output average 2. An 3.A.2 a. Copper vapor lasers having both of the following characteristics: following the of both having lasers vapor Copper 3.A.2 a.

2 or or

or Technical Note: For the purpose of 6A005.a.6.b. Note 2.a., defined ‘brightness’is as the output power divided by the squared of the “laser” Beam i.e., (output Parameter Product power)/BPP (BPP), having a BPP exceeding 24 mm • mrad. • mm 24 exceeding BPP having a having a BPP exceeding 3,5 mm • mrad; • mm 3,5 exceeding BPP having a mrad; • mm 5 a BPP exceeding mrad; • mm 7,2 a BPP exceeding mrad; • mm 12 a BPP exceeding i. Output power exceeding 8 kW but not exceeding 10 kW and kW 10 but not exceeding kW i. 8 Output power exceeding e. Output power exceeding 3,3 kW but not exceeding 4 kW and kW but not exceeding 4 kW Output power exceeding 3,3 e. f. Output power exceeding 4 kW but not 5 kW and exceeding having g. Output power exceeding 5 kW but not 6 kW and exceeding having h. Output power exceeding 6 kW but not 8 kW and exceeding having or 1 W; 1 W; a. Single transverse mode and output power exceeding 50 W; 50 following: exceeding power output and mode transverse a. Single b. Multiple transverse mode and output power exceeding 80 W; 80 exceeding power output and mode transverse b. Multiple a. Output energy exceeding 50 mJ per pulse and “peak power” exceeding 1 W; 1 exceeding power” “peak and pulse per mJ 50 exceeding energy a. Output b. “Average output power” exceeding 1 W; 1 exceeding power” output b. “Average 8. Output wavelength exceeding 1 555 nm and output power exceeding exceeding power output and nm 555 1 exceeding wavelength Output 8. 7. Output wavelength exceeding 1 150 nm but not exceeding 1 555 nm and of the 7. 555 nm but not exceeding 1 150 Output wavelength exceeding 1 1. Output wavelength less than 150 nm and any of the following: the nm and any of 1. than 150 Output wavelength less b. having “pulsed Non-“tunable” any lasers” of the following:

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or or

or or or output power” equal to or less than 50 W. than less or equal to output power” 5 GW; 150 W; 50 W; 1. Output energy exceeding 0,005 J per pulse and “peak power” exceeding power” “peak and pulse per J 0,005 exceeding energy 1. Output 2. “Average output power” exceeding 50 W; 50 exceeding power” output 2. “Average J per pulse and “peak power” exceeding 1. Output energy exceeding 1,5 1. Output energy exceeding 1,5 J per pulse and “peak power” exceeding 1. Output energy exceeding 1,5 W; 150 exceeding power” output 2. “Average 2. “Average output power” exceeding 20 W; 20 exceeding power” output 2. “Average or Note: 6A005.b.2.b. does not control Argon “lasers” having an “average a. “Pulse duration” less than 1 ps and any of the following: the of any following: and ps 1 than less duration” a. “Pulse a. Output energy exceeding 1,5 J per pulse and “peak power” exceeding 30 W; 30 exceeding power” “peak and following: pulse per J 1,5 exceeding energy a. Output b. “Average output power” exceeding 30 W; 30 exceeding power” output b. “Average b. Multiple transverse mode output and any of the following: the of any and output mode transverse b. Multiple b. “Pulse duration” equal to or exceeding 1 ps and any the following: of a. Single transverse mode output and any of the following: the following: of any and output mode transverse a. Single 4. nm and any of the nm but not exceeding 800 Output wavelength exceeding 540 2. nm and any of the but not exceeding 510 more nm or Output wavelength of 150 3. nm and any of the nm but not exceeding 540 Output wavelength exceeding 510

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s and any of the following: the and any of s μ or or or or or W; 5 GW; 50 W; 50 W; 50 W; 80 W; 20 W; 50 W; 20 W; 1. Output energy exceeding 1,5 J per pulse and “peak power” exceeding 30 exceeding power” “peak and pulse per J 1,5 exceeding energy 1. Output 2. “Average output power” exceeding 30 W; 30 exceeding power” output 2. “Average 1. Output energy exceeding 0,005 J per pulse and “peak power” exceeding power” “peak and pulse per J 0,005 exceeding energy 1. Output 3. exceeding output power” mode output and “average transverse Multiple 1. Output J energy per exceeding pulse 2 and “peak power” exceeding output power” exceeding mode output and “average Single transverse 2. 3. exceeding output power” mode output and “average transverse Multiple pulse; per GW 2 exceeding power” “peak 1. Output 2. Single transverse mode output and “average output power” exceeding mode output and “average Single transverse 2. of the following: J per pulse and “peak power” exceeding 1. Output energy exceeding 0,5 output power” exceeding mode output and “average Single transverse 2. a. “Pulse duration” less than 1 ps and any of the following: the of any following: and ps 1 than less duration” a. “Pulse c. “Pulse duration” exceeding 1 exceeding duration” c. “Pulse following: of any and the following: ps, 1 than less of duration” a. “Pulse b. “Pulse duration” equal to or exceeding 1 ps and not exceeding 1 exceeding not and ps 1 exceeding or to equal duration” b. “Pulse 5. nm and any of the nm but not exceeding 975 Output wavelength exceeding 800 6. Output wavelength exceeding 975 nm but not exceeding 1 150 nm and any of 150 nm but not exceeding 1 6. Output wavelength exceeding 975

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 122 s, and any μ or

or or or or or maximum pulse repetition frequency less than or equal to 1 kHz; to equal than or less frequency maximum pulse repetition pulse repetition a at operating of and capable exceeding 100 W than 1 frequency greater kHz; than 1 kHz; frequency greater a pulse repetition exceeding 500 W; a. “Peak power” exceeding 100 MW; 100 exceeding power” a. “Peak a by design to 20 W limited exceeding output power” “Average b. c. ‘Wall-plug efficiency’ exceeding %, 12 “average output power” at operating of capable and W 150 exceeding power” output d. “Average a. “Peak power” exceeding 400 MW; 400 exceeding power” a. “Peak % b. ‘Wall-plug and efficiency’ exceeding “average output 18 power” kW; 2 exceeding power” output c. “Average e. Output energy exceeding 2 J per pulse; per J 2 exceeding energy e. Output pulse; per J 4 exceeding energy d. Output 3. Output energy exceeding 0,002 J per pulse; per J 0,002 exceeding energy 3. Output 2. “Average output power” exceeding 10 W; 10 exceeding power” output 2. “Average following: pulse; per GW 5 exceeding power” “peak 1. Output W; 10 exceeding power” output 2. “Average pulse; per J 0,1 exceeding energy 3. Output of the following: following: the of any and output mode transverse 1. Single 2. following: mode output the and any of transverse Multiple b. to or exceeding 1 ps than 1 ns and any of the duration” equal and “Pulse less c. to or exceeding 1 ns but not equal duration” “Pulse

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 123 or s and any of the following: the s and any of μ s and any of the following: s and any of the following: μ μ or or

or or exceeding 100 W; exceeding 500 W; or or a. “Peak power” exceeding 500 kW; 500 exceeding power” a. “Peak % and b. ‘Wall-plug “average efficiency’ output exceeding 12 power” a. “Peak power” exceeding 1 MW; 1 exceeding power” a. “Peak % and b. ‘Wall-plug “average efficiency’ output exceeding 18 power” c. “Average output power” exceeding 150 W; 150 exceeding power” output c. “Average kW; 2 exceeding power” output c. “Average W; 50 W; 80 W; W; W; 1. Single transverse mode output and any of the following: the of any and output mode transverse 1. Single 2. Multiple transverse mode output and any of the following: the of any and output mode transverse 2. Multiple 1. pulse and “peak power” exceeding 50 W; per J Output energy exceeding 2 50 exceeding power” output “average and output mode transverse 2. Single 3. Multiple transverse mode output and “average output power” exceeding output power” mode output and “average 3. transverse Multiple exceeding output power” mode output and “average 3. transverse Multiple 1. Output energy exceeding 0,5 J per pulse and “peak power” exceeding 50 pulse and “peak power” per J 1. Output energy exceeding 0,5 20 exceeding power” output “average and output mode transverse 2. Single d. “Pulse duration” exceeding 1 b. “Pulse duration” exceeding 1 exceeding duration” b. “Pulse the following: 1 exceeding not duration” a. “Pulse 7. Output wavelength exceeding 1 150 nm but not exceeding 1 555 nm, and any of 555 nm but not exceeding 1 7. 150 Output wavelength exceeding 1

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and 20 W; 2. Average or CW output power less than 20 W. 20 than less power output CW or 2. Average multimode output and a wavelength of 150 nm or more but not exceeding multimode output and a wavelength of 150 than less power” “peak a 600 nm and or all pulse of the per following: J 1,5 than less energy 1. Output or or W; or a. Output energy exceeding 1 J per pulse and “peak power” exceeding 20 W; 20 exceeding power” “peak the following: and pulse per J 1 exceeding energy a. Output a. exceeding 1 W; and “peak power” pulse per exceeding 50 mJ Output energy b. Average or CW output power exceeding 1 W; 1 exceeding power output CW or b. Average a having lasers, liquid other or lasers dye control not does Note: 6A005.c.1. W; 1 exceeding power output CW or b. Average a. Output energy exceeding 50 mJ per pulse and “peak power” exceeding 1 W; 1 exceeding power” “peak and pulse per mJ 50 exceeding energy a. Output b. Average or CW output power exceeding 20 W; 20 exceeding power output CW or b. Average a. Output energy exceeding 100 mJ per pulse and “peak power” exceeding 1 exceeding power” “peak and pulse per mJ 100 exceeding energy a. Output b. “Average output power” exceeding 1 W; 1 exceeding power” output b. “Average 2. Output wavelength of 600 nm or more but not exceeding 1 400 nm, and any of 2. 400 more but not exceeding 1 nm or Output wavelength of 600 8. Output wavelength exceeding 1 555 nm and any of the following: the nm and any of 555 8. Output wavelength exceeding 1 following: the nm and any of 3. 400 Output wavelength exceeding 1 1. Output wavelength less than 600 nm and any of the following: the of any and nm 600 than less wavelength 1. Output c. having any “lasers” “Tunable” of the following:

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connectors (e.g., fibre optic pigtails). optic fibre connectors (e.g., other equipment is determined by the control status of the other equipment. exceeding 15W; exceeding 2,5 W; output power, CW or and average exceeding 100 W; CW output or power, exceeding 25 W; and average exceeding 500 mW; power, exceeding 1 W; power, exceeding 1 power, exceeding 10 W; power, exceeding 1,5 W; the following: nm and average or CW output power, 1. 400 Wavelength of less than 1 2. Wavelength equal to or greater than 1 400 nm and less than 1 900 nm 1. Wavelength of less than 1 400 nm and average or CW output power, 1. 400 Wavelength of less than 1 2. Wavelength equal to or greater than 1 400 nm and less than 1 900 nm 2. Wavelength greater than 1 510 nm and average or CW output power, output CW or average and nm 510 1 than greater 2. Wavelength 3. or CW nm and output average 900 than 1 Wavelength equal to or greater 3. or CW nm and output average 900 than 1 Wavelength equal to or greater 1. Wavelength equal to or less than 1 510 nm and average or CW output CW or average and nm 510 1 following: than less or to equal 1. Wavelength b. Individual, multiple-transverse mode semiconductor “lasers” having any of any having “lasers” semiconductor mode multiple-transverse b. Individual, c. Individual semiconductor “laser” ‘bars’, having any of the following: the of any having ‘bars’, “laser” semiconductor c. Individual Note 1: 6A005.d.1. includes semiconductor “lasers” having optical output Note 2: The control status of semiconductor “lasers” specially designed for a. Individual single-transverse mode semiconductor “lasers” having any of the of any having “lasers” semiconductor mode single-transverse a. Individual 1. Semiconductor “lasers” as follows: as “lasers” 1. Semiconductor d. in not 6A005.a.,specified “lasers”, Other 6A005.b. or 6A005.c. as follows:

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 126 ;

2 ;

2 or ;

;

2 or 2 ;

2 or ;

2 ;

or CW output ‘power density’ greater than 150 W/cm greater CW output ‘power density’ or CW output ‘power density’ greater than 500 or CW W/cm greater output ‘power density’ kW, and having or CW average output ‘power than or equal to 5 less than 350 density’ greater W/cm W; W; 250 W but less than or equal to 500 W, and having average or CW or average and having 500 W, to equal or than less but 250 W 50 W/cm than greater output ‘power density’ 150 W; a. Average or CW output ‘power density’ greater than 50 W/cm 50 than greater density’ following: ‘power output CW or a. Average a. Average or CW total output power less than 250 W and average or average and W 250 than less following: the having any of power output total CW or a. Average b. Average or CW output power greater than 10 W; 10 than greater power output CW or b. Average a. Average or CW total output power less than 3 kW and having average having and kW 3 than less power output total CW or a. Average b. kW but output Average or CW total power equal to or exceeding 3 1,5 exceeding power, output total CW or average coherent c. Spatially e. Spatially coherent average or CW total output power, exceeding 15 exceeding power, output total CW or average coherent e. Spatially b. Average or CW total output power equal to or exceeding b. e. Spatially coherent average or CW total output power, greater than greater power, output total CW or average coherent e. Spatially c. Average or CW total output power exceeding 5 kW; 5 exceeding power output total CW W/cm or 500 c. Average 2 exceeding density’ ‘power pulsed d. Peak W; 500 exceeding power output total CW or W/cm c. Average 500 exceeding density’ ‘power pulsed d. Peak 3. Wavelength greater than or equal to 1 900 nm and having any of the 900 3. than or equal to 1 Wavelength greater 2. nm, and 900 nm but less than 1 400 than or equal to 1 Wavelength greater 1. Wavelength less than 1 400 nm and having any of the following: the of any having following: of the and nm 400 1 than less 1. Wavelength d. Semiconductor “laser” ‘stacked arrays’ (two-dimensional arrays) having any having arrays) (two-dimensional arrays’ ‘stacked “laser” d. Semiconductor

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and

‘bars’ designed to be fabricated into end-to-end stacked linear arrays. ‘stacked arrays’by specified 6A005.d.1.e., that are designed to 6A005.d.1.e. by combined modified are specified be further or ‘stacked arrays’ specified by 6A005.d.1.e., ‘stacked arrays’specified that are not designed by combined to be further or modified are specified 6A005.d.1.d. Note 2: ‘Stacked arrays’, formed by combining semiconductor “laser” Note 3: 6A005.d.1.e. does not control modular assemblies of single arrays’ to form a larger ‘stacked array’; a larger to form arrays’ Note 1: ‘Stacked arrays’, formed by combining semiconductor “laser” Technical Note: For the purposes of 6A005.d.1.d., means ‘power density’ the total “laser” array’.‘stacked surface area of the output power the emitter divided by 4. At least one “laser” ‘bar’ specified in 6A005.d.1.c.; in specified ‘bar’ “laser” one least 4. At 2. and cooling; both electronics connections, common for Integrated 6A005.d.1.d., having all of the following: the of all 6A005.d.1.d., having 1. Specially designed or modified to be combined with other ‘stacked diode ‘bar’) consists of multiple semiconductor diode consists of multiple “lasers” in a one-dimen ‘bar’) sional array. semiconductor “lasers”. array of Technical Notes: 1. Semiconductor are commonly “lasers” “laser” diodes. called or ‘bar’ diode “laser” a ‘bar’, “laser” semiconductor a called (also ‘bar’ 2. A forming a two-dimensional ‘bars’ multiple of consists array’ A ‘stacked 3. e. Semiconductor “laser” ‘stacked arrays’, other than those specified in

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characteristics: nm; 360 and 240 between wavelengths at 1. Operating and Hz; 250 than greater rate repetition 2. A W; 500 than greater power output average 3. An 3.A.2 h. Pulsed excimer lasers (XeF, XeCl, KrF) having all of the following the of all having KrF) XeCl, (XeF, lasers excimer Pulsed 3.A.2 h. or s and any of μ s and any of the μ

or or or or or ) “lasers” having ) “lasers” any of the following: 2

following: kW; 10 exceeding power” output 1. “Average 1. Pulse energy exceeding 5 J per pulse; the following: per J 5 exceeding energy 1. Pulse 2. “Peak power” exceeding 100 kW; 100 exceeding power” 2. “Peak 2. “Average output power” exceeding 2,5 kW; 2,5 exceeding power” output 2. “Average 1. Output energy exceeding 50 mJ per pulse; per mJ 50 exceeding energy 1. Output 2. “Average output power” exceeding 1 W; 1 exceeding power” output 2. “Average the following: pulse; per J 1,5 exceeding energy 1. Output 2. “Average output power” exceeding 120 W; 120 exceeding power” output 2. “Average a. nm and any of the following: Output wavelength not exceeding 150 b. Output wavelength exceeding 150 nm but not exceeding 190 nm and any of nm b. but not exceeding 190 Output wavelength exceeding 150 a. CW output power exceeding 15 kW; 15 exceeding power output a. CW 10 exceeding duration” “pulse a with output b. Pulsed b. Average or CW output power exceeding 5 kW; 5 exceeding power output CW or b. Average c. Pulsed than 10 output with a “pulse duration” equal to or less a. Output energy exceeding 2 J per pulse and “peak power” exceeding 5 kW; 3. Carbon dioxide (CO dioxide 3. Carbon 4. Excimer “lasers” having any of the following: the of any having “lasers” 4. Excimer 2. Carbon monoxide (CO) “lasers” having any of the following: the of any having “lasers” monoxide (CO) 2. Carbon

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) “lasers”; ) “lasers”;

2 or

or or s and output energy exceeding 50 J per s and output energy exceeding 50 μ s and output energy exceeding 100 J per s and output energy exceeding 100 μ -I) “lasers”; -I) “lasers”;

or 3B001. output pulse or that have a time interval between pulses exceeding one between pulses exceeding interval time have a that output pulse or minute. 2. Deuterium Fluoride-Carbon dioxide (DF-CO dioxide Fluoride-Carbon 2. Deuterium pulse; pulse; 1. Oxygen Iodine (O Iodine 1. Oxygen 2. “Average output power” exceeding 500 W; 500 exceeding power” output 2. “Average W; 30 exceeding power” output 2. “Average the following: pulse; per J 10 exceeding energy 1. Output 1. Output energy exceeding 1,5 J per pulse; per J 1,5 exceeding energy 1. Output a. “Pulse duration” not exceeding 1 exceeding not duration” a. “Pulse b. “Pulse duration” exceeding 1 b. Note: ‘Non-repetitive pulsed’ refers to “lasers” that produce either a single a. Hydrogen Fluoride (HF) “lasers”; “lasers”; (HF) Fluoride a. Hydrogen “lasers”; (DF) Fluoride b. Deuterium follows: as lasers” c. “Transfer c. Output wavelength exceeding 190 nm but not exceeding 360 nm and any of c. nm but not exceeding 360 Output wavelength exceeding 190 see equipment, lithography for designed specially “lasers” excimer N.B.: For d. Output wavelength exceeding 360 nm and any of the following: the of any and nm 360 exceeding wavelength d. Output 1. Mirrors cooled either by ‘active cooling’ or by heat pipe cooling; pipe heat by or cooling’ ‘active by either cooled 1. Mirrors 6. ‘Non-repetitive pulsed’ Nd: glass “lasers” having any of the following: the of any having “lasers” glass Nd: pulsed’ 6. ‘Non-repetitive 5. “Chemical lasers” as follows: as lasers” 5. “Chemical e. Components as follows: as e. Components

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and

or exceeding 1,5 mm mrad for a number of input fibres less than or less a number of input fibres for mm mrad exceeding 1,5 equal to 5; a. the output not at Product (BPP) measured A Beam Parameter rated total average or CW output power (excluding output power trans (excluding CW output power or average total rated 000 mitted through W; the single mode core if present) exceeding 1 average or CW output power exceeding 4 600 W; average or CW output power exceeding 4 3. Having any of the following: the of any 3. Having 1. An insertion loss better (less) than or equal to 0,3 dB maintained at a at maintained following: dB 0,3 to equal or than (less) better loss insertion 1. An 2. than equal to or greater Number of input fibres 3; following: total rated a at maintained dB 0,5 than (less) better loss insertion 1. An 2. than 3; equal to or greater Number of input fibres Technical Note: components using flowing optical for cooling technique a is cooling’ ‘Active mm below the optical fluids within the subsurface (nominally less than 1 of the optical component surface) to remove heat from optic. the Note: Fibre combiners and MLDs are specified in 6A005.e.3. in specified are MLDs and combiners Note: Fibre a. Multimode to multimode fused tapered fibre combiners having all of the b. Single mode to multimode fused tapered fibre combiners having all of the optical components, other than combiners fused and tapered fibre Multi-Layer Dielectric gratings (MLDs), specially designed for use with specified “lasers”; 3. Fibre laser components as follows: as components laser 3. Fibre 2. optical or electro- transmissive or partially or transmissive mirrors Optical

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 131 /10 at the /10 at λ

rad; μ or m, whichever is the smaller; the is m, whichever μ

and number of input fibres greater than greater input fibres number of 5; b. A BPP measured at the output not exceeding 2,5 mm mrad for a for mrad mm 2,5 exceeding not output the at measured BPP b. A lasers; 10 kW/cm High Power Laser” (“SHPL”) applications, see the Military Goods Military the applications, see High Power Laser” (“SHPL”) Controls. least 20 % of the beam's wavelength; least 20 least 5 % of the beam's wavelength; 5 least 1. Designed or coherent beam combination for spectral of 5 or more fibre 2. CW Laser Induced Damage Threshold (LIDT) greater than or equal to b. Hz and of at phase discrimination 000 equal to or more than rates 1 Frame of equal to or less than 10 errors beam steering of coherent beam combination to an accuracy system for “SHPL” 0,1 or designed wavelength, a. Frame rates equal to or more than 100 Hz and phase discrimination of at of discrimination phase and Hz 100 following: the and any of wavefront beam 50 positions on a than more or to equal rates a. Frame c. MLDs having all of the following: the of all having c. MLDs 2. “Laser” diagnostic equipment capable of measuring “SHPL” system angular “Laser” 2. Optical equipment and components, specially designed for a phased-array 3. systems; “SHPL” with use for designed specially telescopes 4. Projection N.B.: capable For shared of operating in “Super- elements, aperture optical least mapping of at equipment capable measuring (phase) 1. Dynamic wavefront 1. CW laser output power equal to or exceeding 20 mW; 20 exceeding or to equal power output laser 1. CW f. Optical equipment as follows: as equipment f. Optical g. ‘Laser acoustic detection equipment’ having all of the following: the of all having equipment’ detection acoustic g. ‘Laser

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; and

performance of cameras or imaging devices to meet the character istics below is controlled in 5.D.1 and 5.D.2. follows: N.B.: “Software” specially designed to enhance or release the a. Photocathode area of greater than 20 cm 20 than greater of area a. Photocathode b. Anode pulse rise time of less than 1 ns. 1 than less of time rise pulse b. Anode 5.B.3. as and imaging devices components therefor, High-speed cameras 5.A.1. Photomultiplier tubes having both of the following characteristics: following the of both having tubes 5.A.1. Photomultiplier

and and ;

camera of 6A203.a., or imaging the characteristics device to meet 6A203.b. in 6D203. specified or 6A203.c. is of characteristics performance the of a camera to meet or imaging device 6E203. in specified is 6A203.c or 6A203.a., 6A203.b.

or release the constraints; or release 5. equal to or exceeding 10 Signal to Noise ratio Optical Technical Note: to as a Laser referred sometimes is equipment’detection acoustic ‘Laser Microphone. Detection Flow Particle Microphone or 2. Laser frequency stability equal to or better (less) than 10 MHz; 10 than (less) better or to equal stability frequency 2. Laser nm; 000 not exceeding 2 nm but 000 3. exceeding 1 to or wavelengths equal Laser nm; 1 than (less) better resolution system 4. Optical Note: have they if devices imaging or cameras control not does 6A203.c. 6A203.a. to or to “technology”hardware, “software” the performance less constraints that limit above, provided any of the following: specified they meet than that 1. original manufacturer be returned to the to make the enhancements They need to b. Anode pulse rise time of less than 1 ns. 1 than less of time rise pulse b. Anode a. Photocathode area of greater than 20 cm 20 than greater of area a. Photocathode N.B. 1: “Software” specially designed to enhance or release the performance of a N.B. 2: “Technology”to enhance or release the the form of codes or keys in 2: N.B. 6A203 Cameras and components, other than those specified in 6A003, as follows: as 6A003, in specified those than other components, and 6A203 Cameras 6A202 Photomultiplier tubes having both of the following characteristics: following the of both having tubes 6A202 Photomultiplier

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per second; designed 50ns for specially of or less time gating (shutter) in 5.B.3.b.1 specified cameras or 5.B.3.b.2.; have modular structures and that enable the performance specifi performance enable the and that have modular structures cations in 5.B.3.a.1 or 5.B.3.a.2.; designed cameras and for bearings specially turbines, mirrors specified in 5.B.3.a.1. follows: frames 000 225 than greater rates recording with cameras 1. Framing 2. image exposure time; capable of 50 frame ns or less Framing cameras fast a having devices imaging solid-state and tubes 3. Framing follows: mm/ 0,5 than greater speeds writing with cameras resolution; 1. Streak time less or ns 50 of capable cameras streak 2. Electronic 5.B.3.a.2.; in specified cameras for tubes 3. Streak 4. Plug-ins specially designed for use with streak cameras which 5. Synchronizing electronics units, rotor assemblies consisting of 5.B.3.a a. Streak cameras, and specially designed components therefor, as therefor, components designed specially and cameras, Streak 5.B.3.a a. 5.B.3.b b. Framing cameras and specially designed components therefor as therefor components designed specially and cameras Framing 5.B.3.b b.

s; μ or (shutter) time of 50ns or less specially designed for cameras specified in specified cameras designed of 50ns specially for time or less (shutter) 6A203.b.2.; 6A203.b.1 or structures and that enable the performance specifications in 6A203.a.1. or 6A203.a.2.; 6A203.a.1.; in specified cameras designed for and bearings specially performance to meet the characteristics of 6A203; performance the characteristics to meet enhance of 6A203. or release the performance the characteristics to meet mm/ 0,5 than greater speeds writing with cameras 1. Streak second; per frames 000 225 than greater rates recording with cameras 1. Framing 2. exposure capable of 50 time; Framing cameras ns or less frame 3. Framing tubes and solid-state imaging devices having a fast image gating 2. capable of 50 resolution; cameras ns or less time streak Electronic 6A203.a.2.; in specified cameras for tubes 3. Streak have modular which cameras streak with use designed for specially 4. Plug-ins mirrors turbines, of consisting assemblies rotor units, electronics 5. Synchronizing 2. They require “software” as specified in 6D203 They require “software” as specified to enhance or release the 2. 3. They require “technology” in the form of keys or codes as specified in 6E203 to 6A203 b. Framing cameras, and specially designed components therefor, as follows: as therefor, components designed specially and cameras, Framing 6A203 b. 6A203 a. follows: as designed components therefor, and specially cameras, Streak

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gating (shutter) time of 50 time ns or less; gating (shutter) designed time of 50 ns or less specially gating (shutter) image fast for cameras specified in 5.B.3.c.1.; of 50 time ns or less; gating (shutter) image fast specifications and that enable the performance modular structures in 5.B.3.c.1. have modular structures and that enable the performance specifi performance enable the and that have modular structures cations in 5.B.3.b.1 or 5.B.3.b.2.; designed cameras and bearings specially for turbines, mirrors specified in 5.B.3.b.1 or 5.B.3.b.2. components therefor as follows: as components therefor 1. cameras or electron tube Solid-state cameras with a fast image a having tubes intensifiers image and devices imaging 2. Solid-state a with cells) Pockels or (Kerr devices shuttering 3. Electro-optical 4. Plug-ins specially designed for use with cameras which have 4. Plug-ins specially designed for use with framing cameras which cameras framing with use for designed specially 4. Plug-ins 5. Synchronizing electronics units, rotor assemblies consisting of Technical Note: used alone to produce a single cameras can be frame High speed single such cameras can be combined in or several a dynamic event, image of an images of event. to produce multiple system a sequentially-triggered 5.B.3.c designed and specially tube cameras or electron Solid state c.

time of 50 ns time or less; in specified cameras designed specially for of 50 ns or less time gating (shutter) 6A203.c.1.; of 50 time ns or less; gating (shutter) 6A203.c.1. in specifications performance the enable and that structures and that enable the performance specifications in 6A203.b.1 specifications and that enable the performance or structures 6A203.b.2.; 6A203.b.1 in specified or cameras designed for and bearings specially 6A203.b.2.; follows: 1. Solid-state cameras or electron tube cameras with a fast image gating (shutter) image fast having a tubes intensifiers and image devices imaging 2. Solid-state 3. Electro-optical shuttering devices (Kerr or Pockels cells) with a fast image structures modular have which cameras with use for designed specially 4. Plug-ins 4. Plug-ins specially designed for use with framing cameras which have modular have which cameras framing with use for designed specially 4. Plug-ins mirrors turbines, of consisting assemblies rotor units, electronics 5. Synchronizing Technical Note: In 6A203.b., high speed single frame cameras can be used alone to produce a single image of a dynamic event, or several such cameras can be combined in a sequen system to produce multiple images of an tially-triggered event. 6A203 c. Solid state or electron tube cameras, and specially designed components therefor, as therefor, components designed specially and cameras, tube electron or state Solid 6A203 c.

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Gy (silicon) without operational degradation. operational without Gy (silicon)

1. Operating at wavelengths between 400 and 515 nm; and nm; 515 and 400 between wavelengths at 1. Operating W; 40 than greater power output average 2. An following characteristics: nm; 800 and 300 between wavelengths at 1. Operating W; 1 than greater power output average 2. An and kHz; 1 than greater rate repetition 3. A ns; 100 than less width 4. Pulse or rated as radiation hardened radiation dose to withstand or rated greater a total × 10 than 5 following characteristics: nm; 800 and 300 between wavelengths at 1. Operating W; 30 than greater power output average 2. An Technical Note: to the energy in Joules per kilogram refers The term Gy (silicon) ionizing to exposed when sample silicon unshielded an absorbed by radiation. N.B. See also in correspondence to 6A005 1.A.2. Radiation-hardened TV cameras, or lenses therefor, specially designed specially therefor, lenses or cameras, TV 1.A.2. Radiation-hardened 3.A.2. Lasers, laser amplifiers and oscillators as follows: as oscillators and amplifiers laser 3.A.2. Lasers, 3.A.2.e the of having all and oscillators amplifiers Tunable pulsed dye laser 3.A.2.b Argon ion lasers having both of the following characteristics: following the of both having lasers ion 3.A.2.b Argon 3.A.2.d Tunable pulsed single-mode dye laser oscillators having all of the of all having oscillators laser dye single-mode pulsed 3.A.2.d Tunable

and

rad (silicon)) without operational without rad (silicon)) operational degradation.

6 4. Pulse width less than 100 ns; 100 than less width 4. Pulse Gy(silicon) (5 × 10 Gy(silicon) (5 radiation hardened to withstand a total radiation dose greater than 50 × 10 radiation hardened to withstand a total radiation dose than greater 50 acteristics: acteristics: 1. Operating at wavelengths between 300 nm and W; 800 nm; 1 than greater power output average 2. An kHz; 1 than greater rate repetition 3. A characteristics: 1. Operating at wavelengths between 300 nm and W; 800 nm; 30 than greater power output average 2. An 1. Operating at wavelengths between 400 nm and 515 nm; 2. An average output power greater than 40 W; 40 than greater power output average 2. An Technical Note: to the energy in Joules per kilogram absorbed refers by an The term Gy(silicon) sample when exposed to ionising radiation. unshielded silicon 0B001.h.6.follows: 6A005; as and 6A005.b. see lasers, vapour copper N.B.: For 6A205 a. Argon ion “lasers” having both of the following characteristics: following the of both having “lasers” ion Argon 6A205 a. 6A203 d. designed specially or rated as or lenses therefor, Radiation-hardened TV cameras, 6A205 c. Tunable pulsed dye laser amplifiers and oscillators, having all of the following the of all having oscillators, and amplifiers laser dye pulsed Tunable 6A205 c. 6A205 b. Tunable pulsed single-mode dye laser oscillators having all of the following char following the of all having oscillators laser dye single-mode pulsed Tunable 6A205 b. 6A205 “Lasers”, “laser” amplifiers and oscillators, other than those specified in 0B001.g.5., in specified those than other oscillators, and amplifiers “laser” 6A205 “Lasers”,

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lasers used in applications such as cutting

and welding, as these latter lasers are either continuous wave or continuous wave either are lasers latter these as and welding, are pulsed than with a pulse width 200 greater ns. 5 kW) industrial CO greater than 40 greater W; or than 50 greater W; greater than 1 ns, and having either of the following: output power average an a. mode output with single-transverse A power output average an with output mode multiple-transverse b. A or output nm greater with an average power of between 500 and 550 than 40 W; wavelength and at a repetition rate greater than 250 Hz. than 250 greater rate repetition a wavelength and at 1. Operating at wavelengths between 9 000 and 11 000 nm; 000 11 and 000 9 between wavelengths at 1. Operating Hz; 250 than greater rate repetition 2. A and W; 500 than greater power output average 3. An ns; 200 than less of width 4. Pulse to 1 (typically power higher the control not does 3.A.2.g. Note: Item 3. A repetition rate greater than 1 kHz; and kHz; 1 than greater rate repetition 3. A ns; 100 than less width 4. Pulse oscillators. mode single control not does 3.A.2.e. Note: Item between 1 000 and 1 100 nm having either of the following: 1. Pulse-excited and Q-switched with a pulse duration equal to or 2. Incorporating frequency doubling to give an output wavelength 3.A.2.g the following characteristics: of having all Pulsed carbon dioxide lasers 3.A.2.i. Para-hydrogen Raman shifters designed to operate at 16 mm output mm 16 at operate to designed shifters Raman 3.A.2.i. Para-hydrogen 3.A.2.c. Neodymium-doped (other than glass) lasers with an output wavelength output an with lasers glass) than (other 3.A.2.c. Neodymium-doped m output wavelength μ

and and

40 W; or 40 W; W; or and having either of the following: the of and having either a. than greater output power average an output with mode single–transverse A 50 than greater power average an having output mode multiple-transverse b. A than 40 W; more output power of an average nm with and 550 and at a repetition rate greater than 250 Hz; than 250 greater rate repetition a and at ns, 1 than more 1 000 or and to 1 100 nm having equal either duration of pulse the a following with Q-switched and 1. Pulse-excited 2. frequency doubling Incorporating to give an output wavelength between 500 4. Pulse width of less than 200 ns; 200 than less of width 4. Pulse 1. Operating at wavelengths between 000 nm 9 Hz; and 11 000 nm; 250 than greater rate repetition 2. A W; 500 than greater power output average 3. An 4. Pulse width less than 100 ns; 100 than less width 4. Pulse 3. A repetition rate greater than 1 kHz; 1 than greater rate repetition 3. A Note: 6A205.c. does not control single mode oscillators; 6A205 f. Neodymium-doped (other than glass) “lasers” with an output wavelength between wavelength output an with “lasers” glass) than (other Neodymium-doped 6A205 f. 6A205 e. Para-hydrogen Raman shifters designed to operate at 16 at operate to designed shifters Raman Para-hydrogen 6A205 e. 6A205 d. the following characteristics: of having all Pulsed carbon dioxide “lasers”

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 137

); 2

(Velocity Interferometer Systems Any for DLIs Reflector), (Velocity Interferometer and PDV (Photonic Doppler Interferometers) (Doppler Laser Velocimeters) also known as Het-V (Heterodyne Velocimeters). 5 kW) industrial CO lasers used in applications such as cutting such as applications used in CO lasers kW) industrial 5 or continuous wave either are lasers latter these as and welding, are pulsed than with a pulse width 200 greater ns 10 GPa, including gauges made with manganin, ytterbium, and manganin, ytterbium, with gauges made including 10 GPa, PVF (PVBF, polyvinylidene bifluoride during time intervals of less than 10 ms; 10 than less of intervals during time Note: Item 5.B.5.a. includes velocity interferometers such as VISARs as such interferometers 5.B.5.a. velocity includes Note: Item istics: 1. Operating at wavelengths between 5 000 Hz; and 6 000 nm; 250 than greater rate repetition 2. A and W; 200 than greater power output average 3. An ns; 200 than less of width 4. Pulse 1 to (typically power higher the control 3.A.2.j. not does Note: Item km/s for a. Velocity measuring interferometers velocities exceeding 1 3.A.2.j Pulsed carbon monoxide of the following character having all lasers 5.B.5.a Specialized instrumentation for hydrodynamic experiments, as follows: as experiments, hydrodynamic for instrumentation 5.B.5.a Specialized 5.B.5.c. c. Quartz pressure transducers for pressures greater than 10 GPa. 10 than greater pressures for transducers pressure Quartz 5.B.5.c. c. 5.B.5.b. b. Shock pressure gauges capable of measuring pressures greater than greater pressures measuring of capable gauges pressure Shock 5.B.5.b. b. and

); 2

Systems for Any Reflector), DLIs (Doppler Laser Interferometers) and PDV DLIs (Doppler Laser Interferometers) Systems for Any Reflector), also known Veloci (Heterodyne as Het-V (Photonic Doppler Velocimeters) meters). 4. Pulse width of less than 200 ns. 200 than less of width 4. Pulse all of the following: 1. Operating at wavelengths between 5 000 Hz; and 6 000 nm; 250 than greater rate repetition 2. A W; 200 than greater power output average 3. An 10 GPa, including gauges made with manganin, ytterbium, and polyvinylidene and manganin, ytterbium, including gauges made with 10 GPa, bifluoride (PVBF, PVF b. Quartz pressure transducers for pressures greater than 10 GPa. 10 than greater pressures for transducers pressure b. Quartz a. Shock pressure gauges capable of measuring pressures greater than Note: 6A225 includes velocity interferometers such as VISARs (Velocity Interferometer (Velocity VISARs as such interferometers velocity includes Note: 6A225 intervals of less than 10 microseconds. 6A226 Pressure sensors, as follows: as sensors, 6A226 Pressure 6A205 g. in 6A005.d.2.,than those specified other Pulsed carbon monoxide having lasers, 6A225 Velocity interferometers for measuring velocities exceeding 1 km/s during time during km/s 1 exceeding velocities measuring for interferometers 6A225 Velocity

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“production” or “use” of equipment, material or “software” specified in 5.A. specified or “software” “production” or “use” of equipment, material through 5.D. “production” or “use” of equipment, material or “software” specified in 5.A. specified or “software” “production” or “use” of equipment, material through 5.D. the performance characteristics of equipment controlled in Item 5.B.3. of equipment in Item controlled characteristics the performance Nuclear Suppliers Group's as in control list INFCIRC/254/Rev.9/Part2 Nuclear Suppliers Group's as in control list INFCIRC/254/Rev.9/Part2 5.D.1. “Technology” according to the Technology Controls for the “development”, 5.D.1. “Technology” according to the Technology Controls for the “development”, 5.D.2. “Software” or encryption keys/codes specially designed to enhance or release or enhance to designed specially keys/codes encryption or 5.D.2. “Software” transit of dual-use items transit of dual-use items equipment specified in 6A003, in 6A005.a.2., equipment specified 6A005.b.2., 6A005.b.3., 6A005.d.3.c., 6A005.d.4.c., 6A202, 6A005.b.4., 6A005.b.6., 6A005.c.2., 6A226. 6A203, 6A205, 6A225 or performance of cameras or imaging devices to meet the characteristics of or imaging of cameras devices performance to meet the characteristics 6A203.c. 6A203a. to cameras or imaging devices to meet the characteristics of 6A203.a. or imaging cameras devices to to meet the characteristics 6A203.c.

6E201 “Technology” according to the General Technology Note for the “use” of “use” the for Note Technology General the to according 6E201 “Technology” 6E203 the release codes or keys, to enhance “Technology”,or form of in the 6D203 “Software” specially designed to enhance or release the performance of performance the release or enhance to designed specially 6D203 “Software” 2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and brokering exports, transfer, of control the for 5 Community 2009 of regime a up May 2009 setting 2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and brokering exports, transfer, of control the for 5 Community 2009 of regime a up May 2009 setting The corresponding Council No 428/ in systems, equipment Regulation (EC) and components identified as The corresponding Council No 428/ in systems, equipment Regulation (EC) and components identified as 6E Technology 6D Software M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 139

▼M24 ANNEX II

List of other goods and technology, including software, referred to in Article 3a

INTRODUCTORY NOTES 1. Unless otherwise stated, reference numbers used in the column entitled “Description” refer to the descriptions of dual-use items set out in Annex I to Regulation (EC) No 428/2009.

2. A reference number in the column entitled “Related item from Annex I to Regulation (EC) No 428/2009” means that the characteristics of the item described in the column “Description” lie outside the parameters set out in the description of the dual-use entry referred to.

3. Definitions of terms between ‘single quotation marks’ are given in a technical note to the relevant item.

4. Definitions of terms between “double quotation marks” can be found in Annex I to Regulation (EC) No 428/2009.

GENERAL NOTES 1. The object of the controls contained in this Annex should not be defeated by the export of any non-controlled goods (including plant) containing one or more controlled components when the controlled component or components are the principal element of the goods and can feasibly be removed or used for other purposes.

N.B.: In judging whether the controlled component or components are to be considered the principal element, it is necessary to weigh the factors of quantity, value and technological know-how involved and other special circumstances which might establish the controlled component or components as the principal element of the goods being procured.

2. The goods specified in this Annex include both new and used goods.

GENERAL TECHNOLOGY NOTE (GTN) (To be read in conjunction with section II.B.)

1. The sale, supply, transfer or export of “technology” which is “required” for the “development”, “production” or “use” of goods the sale, supply, transfer or export of which is controlled in Part A (Goods) below, is controlled in accordance with the provisions of Section II.B.

2. The “technology” “required” for the “development”, “production” or “use” of goods under control remains under control even when applicable to non- controlled goods.

3. Controls do not apply to that “technology” which is the minimum necessary for the installation, operation, maintenance (checking) and repair of those goods which are not controlled or the export of which has been authorised in accordance with Regulation (EC) No 423/2007 or this Regulation.

4. Controls on “technology” transfer do not apply to information “in the public domain”, to “basic scientific research” or to the minimum necessary information for patent applications. 02012R0267 — EN — 18.01.2017 — 022.003 — 140

▼M24 II.A. GOODS

A0. Nuclear Materials, Facilities, and Equipment

Related item from Annex I to No Description Regulation (EC) No 428/2009

II.A0.001 Hollow cathode lamps as follows: — a. Iodine hollow cathode lamps with windows in pure silicon or quartz b. Uranium hollow cathode lamps

II.A0.002 Faraday isolators in the wavelength range 500 nm – 650 nm —

II.A0.003 Optical gratings in the wavelength range 500 nm – 650 nm —

II.A0.004 Optical fibres in the wavelength range 500 nm – 650 nm coated with anti- — reflecting layers in the wavelength range 500 nm – 650 nm and having a core diameter greater than 0,4 mm but not exceeding 2 mm

II.A0.005 Nuclear reactor vessel components and testing equipment, other than those 0A001 specified in 0A001, as follows: 1. Seals 2. Internal components 3. Sealing, testing and measurement equipment

II.A0.006 Nuclear detection systems for detection, identification or quantification of 0A001.j radioactive materials and radiation of nuclear origin and specially designed components thereof other than those specified in 0A001.j. or 1A004.c. 1A004.c

II.A0.007 Bellows-sealed valves made of aluminium alloy or stainless steel type 0B001.c.6 304, 304L or 316L. 2A226 Note: This item does not cover bellow valves defined in 0B001.c.6 and 2A226.

II.A0.008 Laser mirrors, other than those specified in 6A005.e, consisting of 0B001.g.5, 6A005.e – 6 – 1 substrates having a thermal expansion coefficient of 10 K or less at 20 °C (e.g. fused silica or sapphire). Note: This item does not cover optical systems specially designed for astronomical applications, except if the mirrors contain fused silica.

II.A0.009 Laser lenses, other than those specified in 6A005.e.2, consisting of 0B001.g, 6A005.e.2 – 6 – 1 substrates having a thermal expansion coefficient of 10 K or less at 20 °C (e.g. fused silica).

II.A0.010 Pipes, piping, flanges, fittings made of, or lined with, nickel or nickel 2B350 alloy containing more than 40 % nickel by weight, other than those specified in 2B350.h.1. 02012R0267 — EN — 18.01.2017 — 022.003 — 141

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Related item from Annex I to No Description Regulation (EC) No 428/2009

II.A0.011 Vacuum pumps other than those specified in 0B002.f.2 or 2B231, as 0B002.f.2, 2B231 follows: Turbomolecular pumps having a flowrate equal to or greater than 400 l/s, Roots type vacuum roughing pumps having a volumetric aspiration 3 flowrate greater than 200 m /h. Bellows-sealed, scroll, dry compressor, and bellows-sealed, scroll, dry vacuum pumps.

II.A0.012 Shielded enclosures for the manipulation, storage and handling of radio 0B006 active substances (Hot cells).

II.A0.013 ‘Natural uranium’ or ‘depleted uranium’ or thorium in the form of metal, 0C001 alloy, chemical compound or concentrate and any other material containing one or more of the foregoing, other than those specified in 0C001.

II.A0.014 Detonation chambers having a capacity of explosion absorption of more — than 2.5 kg TNT equivalent.

II.A0.015 ‘Glove Boxes’, specially designed for radioactive isotopes, radioactive 0B006 sources or radionuclides. Technical Note: ‘Glove Boxes’ means equipment providing protection to the user, from hazardous vapour, particles or radiation, from materials inside the equipment being handled or processed by a person outside the equipment, by means of manipulators or gloves integrated into the equipment.

II.A0.016 Toxic gas monitoring systems designed for continuous operation and 0A001 detection of Hydrogen Sulphide, and specially designed detectors therefore. 0B001.c

II.A0.017 Helium Leak Detectors. 0A001 0B001.c

A1. aterials, chemicals, ‘microorganisms’ and ‘toxins’

Related item from Annex I to No Description Regulation (EC) No 428/2009

II.A1.001 Bis(2-ethylhexyl) phosphoric acid (HDEHP or D2HPA) CAS 298-07-7 — solvent in any quantity, with a purity greater than 90 %.

II.A1.002 Fluorine gas (Chemical Abstract Number (CAS): 7782-41-4), with a — purity of at least 95 %. 02012R0267 — EN — 18.01.2017 — 022.003 — 142

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Related item from Annex I to No Description Regulation (EC) No 428/2009

II.A1.003 Ring-shaped seals and gaskets, having an inner diameter of 400 mm or — less, made of any of the following materials: a. Copolymers of vinylidene fluoride having 75 % or more beta crystalline structure without stretching; b. Fluorinated polyimides containing 10 % by weight or more of combined fluorine; c. Fluorinated phosphazene elastomers containing 30 % by weight or more of combined fluorine; d. Polychlorotrifluoroethylene (PCTFE, e.g. Kel-F ®); e. Fluoro-elastomers (e.g., Viton ®, Tecnoflon ®); f. Polytetrafluoroethylene (PTFE).

II.A1.004 Personal equipment for detecting radiation of nuclear origin, including 1A004.c personal dosimeters. Note: This item does not cover nuclear detection systems defined in item 1A004.c.

II.A1.005 Electrolytic cells for fluorine production with an output capacity greater 1B225 than 100 g of fluorine per hour. Note: This item does not cover electrolytic cells defined in item 1B225.

II.A1.006 Catalysts, other than those prohibited by 1A225, containing platinum, 1B231, 1A225 palladium or rhodium, usable for promoting the hydrogen isotope exchange reaction between hydrogen and water for the recovery of tritium from heavy water or for the production of heavy water.

II.A1.007 Aluminium and its alloys, other than those specified in 1C002.b.4 or 1C002.b.4, 1C202.a 1C202.a, in crude or semi-fabricated form having either of the following characteristics: a. Capable of an ultimate tensile strength of 460 MPa or more at 293 K (20 °C); or b. Having a tensile strength of 415 MPa or more at 298 K (25 °C).

II.A1.008 Magnetic metals, of all types and of whatever form, having an initial 1C003.a relative permeability of 120 000 or more and a thickness between 0,05 and 0,1 mm.

II.A1.009 ‘Fibrous or filamentary materials’ or prepregs, as follows: 1C010.a N.B. SEE ALSO II.A1.019.A. 1C010.b a. Carbon or aramid ‘fibrous or filamentary materials’ having either of the 1C210.a following characteristics: 1C210.b 6 1. A ‘specific modulus’ exceeding 10 × 10 m; or 4 2. A ‘specific tensile strength’ exceeding 17 × 10 m; b. Glass ‘fibrous or filamentary materials’ having either of the following characteristics: 6 1. A ‘specific modulus’ exceeding 3,18 × 10 m; or 3 2. A ‘specific tensile strength’ exceeding 76,2 × 10 m; c. Thermoset resin-impregnated continuous ‘yarns’, ‘rovings’, ‘tows’ or ‘tapes’ with a width of 15 mm or less (once prepregs), made from 02012R0267 — EN — 18.01.2017 — 022.003 — 143

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Related item from Annex I to No Description Regulation (EC) No 428/2009

carbon or glass ‘fibrous or filamentary materials’ other than those specified in II.A1.010.a. or b. Note: This item does not cover ‘fibrous or filamentary materials’ defined in items 1C010.a, 1C010.b, 1C210.a and 1C210.b.

II.A1.010 Resin-impregnated or pitch-impregnated fibres (prepregs), metal or 1C010.e. carbon-coated fibres (preforms) or ‘carbon fibre preforms’, as follows: 1C210 a. Made from ‘fibrous or filamentary materials’ specified in II.A1.009 above; b. Epoxy resin ‘matrix’ impregnated carbon ‘fibrous or filamentary materials’ (prepregs), specified in 1C010.a, 1C010.b or 1C010.c, for the repair of aircraft structures or laminates, of which the size of individual sheets does not exceed 50 cm × 90 cm; c. Prepregs specified in 1C010.a, 1C010.b or 1C010.c, when impregnated with phenolic or epoxy resins having a glass transition temperature (Tg) less than 433 K (160 °C) and a cure temperature lower than the glass transition temperature. Note: This item does not cover ‘fibrous or filamentary materials’ defined in item 1C010.e.

II.A1.011 Reinforced silicon carbide ceramic composites usable for nose tips, re- 1C107 entry vehicles, nozzle flaps, usable in ‘missiles’, other than those specified in 1C107.

II.A1.012 Maraging steels, other than those specified in 1C116 or 1C216, ‘capable 1C216 of’ an ultimate tensile strength of 2 050 MPa or more, at 293 K (20 °C). Technical Note: The phrase ‘maraging steel capable of’ encompasses maraging steel before or after heat treatment.

II.A1.013 Tungsten, tantalum, tungsten carbide, tantalum carbide and alloys, having 1C226 both of the following characteristics: a. In forms having a hollow cylindrical or spherical symmetry (including cylinder segments) with an inside diameter between 50 mm and 300 mm; and b. A mass greater than 5 kg. Note: This item does not cover tungsten, tungsten carbide and alloys defined in item 1C226.

II.A1.014 Elemental powders of cobalt, neodymium or samarium or alloys or — mixtures thereof containing at least 20 % by weight of cobalt, neodymium or samarium, with a particle size less than 200 μm. 02012R0267 — EN — 18.01.2017 — 022.003 — 144

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Related item from Annex I to No Description Regulation (EC) No 428/2009

II.A1.015 Pure tributyl phosphate (TBP) [CAS No 126-73-8] or any mixture having — a TBP content of more than 5 % by weight.

II.A1.016 Maraging steel, other than those prohibited by 1C116, 1C216 or II.A1.012 — Technical Note: Maraging steels are iron alloys generally characterised by high nickel, very low carbon content and the use of substitutional elements or precipitates to produce strengthening and age-hardening of the alloy.

II.A1.017 Metals, metal powders and material as follows: — a. Tungsten and tungsten alloys, other than those prohibited by 1C117, in the form of uniform spherical or atomized particles of 500 μm diameter or less with a tungsten content of 97 % by weight or more; b. Molybdenum and molybdenum alloys, other than those prohibited by 1C117, in the form of uniform spherical or atomized particles of 500 μm diameter or less with a molybdenum content of 97 % by weight or more; c. Tungsten materials in the solid form, other than those prohibited by 1C226, or II.A1.013 having material compositions as follows: 1. Tungsten and alloys containing 97 % by weight or more of tungsten; 2. Copper infiltrated tungsten containing 80 % by weight or more of tungsten; or 3. Silver infiltrated tungsten containing 80 % by weight or more of tungsten.

II.A1.018 Soft magnetic alloys having a chemical composition as follows: — (a) Iron content between 30 % and 60 %, and (b) Cobalt content between 40 % and 60 %.

II.A1.019 “Fibrous or filamentary materials” or prepregs, not prohibited by Annex I — or by Annex II (under II.A1.009, II.A1.010) of this Regulation, or not specified by Annex I of Regulation (EC) No 428/2009, as follows: (a) Carbon “fibrous or filamentary materials“; Note: II.A1.019a. does not cover fabrics. (b) Thermoset resin-impregnated continuous “yarns”, “rovings”, “tows”, or “tapes”, made from carbon “fibrous or filamentary materials”; (c) Polyacrylonitrile (PAN) continuous “yarns”, “rovings”, “tows” or “tapes” 02012R0267 — EN — 18.01.2017 — 022.003 — 145

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Related item from Annex I to No Description Regulation (EC) No 428/2009

II.A1.020 Steel alloys in sheet or plate form, having any of the following char 1C116 acteristics: 1C216 (a) Steel alloys ‘capable of’ ultimate tensile strength of 1 200 MPa or more, at 293 K (20 °C); or (b) Nitrogen-stabilised duplex stainless steel. Note: The phrase alloys ‘capable of’ encompasses alloys before or after heat treatment Technical Note: ‘Nitrogen-stabilised duplex stainless steel’ has a two-phase microstructure consisting of grains of ferritic and austenitic steel with the addition of nitrogen to stabilise the microstructure.

II.A1.021 Carbon-Carbon Composite material. 1A002.b.1

II.A1.022 Nickel alloys in crude or semi-fabricated form, containing 60 % by weight 1C002.c.1.a or more nickel.

II.A1.023 Titanium alloys in sheet or plate form ‘capable of’ an ultimate tensile 1C002.b.3 strength of 900 MPa or more at 293 K (20 °C). Note: The phrase alloys ‘capable of’ encompasses alloys before or after heat treatment.

II.A1.024 Propellants and constituent chemicals for propellants as follows: 1C111 (a) Toluene Diisocyanate (TDI) (b) Methyl Diphenyl Diisocyanate (MDI) (c) Isophorone Diiscocyanate (IPDI) (d) Sodium Perchlorate (e) Xylidine (f) Hydroxy Terminated Polyether (HTPE) (g) Hydroxy Terminated Caprolactone Ether (HTCE) Technical Note: This item refers to pure substance and any mixture containing at least 50 % of one of the chemicals mentioned above.

II.A1.025 ‘Lubricating materials’ containing, as their principal ingredients, any of 1C006 the following: (a) Perfluoroalkylether, (CAS 60164-51-4); (b) Perfluoropolyalkylether, PFPE, (CAS 6991-67-9). ‘Lubricating materials’ means oils and fluids.

II.A1.026 Beryllium-Copper or Copper-Beryllium Alloys in plate, sheet, strip or 1C002.b rolled bar form, having a composition comprising Copper as the major element by weight and other elements including less than 2 % by weight Beryllium. 02012R0267 — EN — 18.01.2017 — 022.003 — 146

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A2. Materials Processing

Related item from Annex I to No Description Regulation (EC) No 428/2009

II.A2.001 Vibration test systems, equipment and components thereof, other than 2B116 those specified in 2B116: a. Vibration test systems employing feedback or closed loop techniques and incorporating a digital controller, capable of vibrating a system at an acceleration equal to or greater than 0,1 g rms between 0,1 Hz and 2 kHz and imparting forces equal to or greater than 50 kN, measured ‘bare table’; b. Digital controllers, combined with specially designed vibration test ‘software’, with a real-time bandwidth greater than 5 kHz designed for use with vibration test systems specified in a.; c. Vibration thrusters (shaker units), with or without associated amplifiers, capable of imparting a force equal to or greater than 50 kN, measured ‘bare table’, and usable in vibration test systems specified in a.; d. Test piece support structures and electronic units designed to combine multiple shaker units in a system capable of providing an effective combined force equal to or greater than 50 kN, measured ‘bare table’, and usable in vibration systems specified in a. Technical Note: ‘Bare table’ means a flat table, or surface, with no fixture or fittings.

II.A2.002 Machine tools and components and numerical controls for machine tools, 2B201.b as follows: 2B001.c a. Machine tools for grinding having positioning accuracies with “all compensations available” equal to or less (better) than 15 μm according to ISO 230/2 (1988) (1) or national equivalents along any linear axis; Note: This item does not cover machine tools for grinding defined in items 2B201.b and 2B001.c. b. Components and numerical controls, specially designed for machine tools specified in 2B001, 2B201, or under a.

II.A2.003 Balancing machines and related equipment as follows: 2B119 a. Balancing machines, designed or modified for dental or other medical equipment, having all the following characteristics: 1. Not capable of balancing rotors/assemblies having a mass greater than 3 kg; 2. Capable of balancing rotors/assemblies at speeds greater than 12 500 rpm; 3. Capable of correcting imbalance in two planes or more; and 02012R0267 — EN — 18.01.2017 — 022.003 — 147

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Related item from Annex I to No Description Regulation (EC) No 428/2009

4. Capable of balancing to a residual specific imbalance of 0,2 g × mm per kg of rotor mass; b. Indicator heads designed or modified for use with machines specified in a. above. Technical Note: Indicator heads are sometimes known as balancing instrumentation.

II.A2.004 Remote manipulators that can be used to provide remote actions in radio 2B225 chemical separation operations or hot cells, other than those specified in 2B225, having either of the following characteristics: a. A capability of penetrating a hot cell wall of 0,3 m or more (through the wall operation); or b. A capability of bridging over the top of a hot cell wall with a thickness of 0,3 m or more (over the wall operation).

II.A2.006 Furnaces capable of operation at temperatures above 400 °C as follows: 2B226 a. Oxidation furnaces 2B227 b. Controlled atmosphere heat treatment furnaces Note: This item does not cover tunnel kilns with roller or car conveyance, tunnel kilns with conveyor belt, pusher type kilns or shuttle kilns, specially designed for the production of glass, tableware ceramics or structural ceramics.

II.A2.007 “Pressure transducers”, other than those defined in 2B230, capable of 2B230 measuring absolute pressures at any point in the range 0 to 200 kPa and having both of the following characteristics: a. Pressure sensing elements made of or protected by “Materials resistant to corrosion by uranium hexafluoride (UF6 )”, and b. Having either of the following characteristics: 1. A full scale of less than 200 kPa and an “accuracy” of better than ± 1 % of full scale; or 2. A full scale of 200 kPa or greater and an “accuracy” of better than 2 kPa.

II.A2.008 Liquid-liquid contacting equipment (mixer-settlers, pulsed columns, 2B350.e centrifugal contactors); and liquid distributors, vapour distributors or liquid collectors designed for such equipment, where all surfaces that come in direct contact with the chemical(s) being processed are made from the following materials: N.B. SEE ALSO II.A2.014 1. Stainless steel. Note: for stainless steel with more than 25 % nickel and 20 % chromium by weight see entry II.A2.014.a

II.A2.009 Industrial equipment and components, other than those specified in 2B350.d 2B350.d, as follows: 02012R0267 — EN — 18.01.2017 — 022.003 — 148

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N.B. SEE ALSO II.A2.015 Heat exchangers or condensers with a heat transfer surface area greater than 2 2 0,05 m , and less than 30 m ; and tubes, plates, coils or blocks (cores) designed for such heat exchangers or condensers, where all surfaces that come in direct contact with the fluid(s) are made from the following materials: 1. Stainless steel. Note 1: for stainless steel with more than 25 % nickel and 20 % chromium by weight see entry II.A2.015a Note 2: This item does not cover vehicle radiators. Technical Note: The materials used for gaskets and seals and other implementation of sealing functions do not determine the status of control of the heat exchanger.

II.A2.010 Multiple-seal, and seal-less pumps, other than those specified in 2B350.i, 2B350.i suitable for corrosive fluids, with manufacturer's specified maximum flow- 3 rate greater than 0,6 m /hour, or vacuum pumps with manufacturer's 3 specified maximum flow-rate greater than 5 m /hour [measured under standard temperature (273 K or 0 °C) and pressure (101,3 kPa) conditions]; and casings (pump bodies), preformed casing liners, impellers, rotors or jet pump nozzles designed for such pumps, in which all surfaces that come in direct contact with the chemical(s) being processed are made from the following materials: N.B. SEE ALSO II.A2.016 1. Stainless steel; Note: for stainless steel with more than 25 % nickel and 20 % chromium by weight see entry II.A2.016a Technical Note: The materials used for gaskets and seals and other implementation of sealing functions do not determine the status of control of the pump.

II.A2.011 Centrifugal separators, capable of continuous separation without the 2B352.c propagation of aerosols and manufactured from: 1. Alloys with more than 25 % nickel and 20 % chromium by weight; 2. Fluoropolymers; 3. Glass (including vitrified or enamelled coating or glass lining); 4. Nickel or alloys with more than 40 % nickel by weight; 5. Tantalum or tantalum alloys; 02012R0267 — EN — 18.01.2017 — 022.003 — 149

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6. Titanium or titanium alloys; or 7. Zirconium or zirconium alloys. Note: This item does not cover centrifugal separators defined in item 2B352.c.

II.A2.012 Sintered metal filters made of nickel or nickel alloy with more than 40 % 2B352.d nickel by weight. Note: This item does not cover filters defined in item 2B352.d.

II.A2.013 Spin-forming machines and flow-forming machines, other than those — controlled by 2B009, 2B109 or 2B209, having a roller force of more than 60 kN and specially designed components therefor. Technical Note: For the purpose of II.A2.013, machines combining the functions of spin- forming and flow-forming are regarded as flow-forming machines.

II.A2.014 Liquid-liquid contacting equipment (mixer-settlers, pulsed columns, 2B350.e centrifugal contactors); and liquid distributors, vapour distributors or liquid collectors designed for such equipment where all surfaces that come in direct contact with the chemical(s) being processed are any of the following: N.B. SEE ALSO II.A2.008. a. Made from any of the following materials: 1. Alloys with more than 25 % nickel and 20 % chromium by weight; 2. Fluoropolymers; 3. Glass (including vitrified or enamelled coating or glass lining); 4. Graphite or ‘carbon graphite’; 5. Nickel or alloys with more than 40 % nickel by weight; 6. Tantalum or tantalum alloys; 7. Titanium or titanium alloys; or 8. Zirconium or zirconium alloys; or b. Made from both stainless steel and one or more of the materials specified in II.A2.014.a. Technical Note: ‘Carbon graphite’ is a composition consisting of amorphous carbon and graphite, in which the graphite content is 8 % or more by weight.

II.A2.015 Industrial equipment and components, other than those specified in 2B350.d 2B350.d, as follows: N.B. SEE ALSO II.A2.009. Heat exchangers or condensers with a heat transfer surface area greater 2 2 than 0,05 m , and less than 30 m ; and tubes, plates, coils or blocks (cores) designed for such heat exchangers or condensers, where all surfaces that come in direct contact with the fluid(s) are any of the follow ing: 02012R0267 — EN — 18.01.2017 — 022.003 — 150

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Related item from Annex I to No Description Regulation (EC) No 428/2009

a. Made from any of the following materials: 1. Alloys with more than 25 % nickel and 20 % chromium by weight; 2. Fluoropolymers; 3. Glass (including vitrified or enamelled coating or glass lining); 4. Graphite or ‘carbon graphite’; 5. Nickel or alloys with more than 40 % nickel by weight; 6. Tantalum or tantalum alloys; 7. Titanium or titanium alloys; 8. Zirconium or zirconium alloys; 9. Silicon carbide; or 10. Titanium carbide; or b. Made from both stainless steel and one or more of the materials specified in II.A2.015.a. Note: This item does not cover vehicle radiators. Technical Note: The materials used for gaskets and seals and other implementation of sealing functions do not determine the status of control of the heat exchanger.

II.A2.016 Multiple-seal, and seal-less pumps, other than those specified in 2B350.i, 2B350.i suitable for corrosive fluids, with manufacturer's specified maximum flow- 3 rate greater than 0,6 m /hour, or vacuum pumps with manufacturer's 3 specified maximum flow-rate greater than 5 m /hour [measured under standard temperature (273 K or 0 °C) and pressure (101,3 kPa) conditions]; and casings (pump bodies), preformed casing liners, impellers, rotors or jet pump nozzles designed for such pumps, in which all surfaces that come in direct contact with the chemical(s) being processed are any of the following: NB. SEE ALSO II.A2.010. a. Made from any of the following materials: 1. Alloys with more than 25 % nickel and 20 % chromium by weight; 2. Ceramics; 3. Ferrosilicon; 4. Fluoropolymers; 5. Glass (including vitrified or enamelled coatings or glass lining); 6. Graphite or ‘carbon graphite’ 7. Nickel or alloys with more than 40 % nickel by weight; 8. Tantalum or tantalum alloys; 9. Titanium or titanium alloys; 10. Zirconium or zirconium alloys; 02012R0267 — EN — 18.01.2017 — 022.003 — 151

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11. Niobium (columbium) or niobium alloys; or 12. Aluminium alloys; or b. Made from both stainless steel and one or more of the materials specified in II.A2.016.a. Technical Note: The materials used for gaskets and seals and other implementation of sealing functions do not determine the status of control of the pump.

II.A2.017 Electrical Discharge Machine (EDM) tools for removing or cutting metals, 2B001.d ceramics or “composites”, as follows, and specially designed ram, sinker or wire electrodes therefor: (a) Ram or sinker electrode Electrical Discharge Machines; (b) Wire electrode Electrical Discharge Machines. Note: Electrical Discharge Machines are also known as Spark Erosion Machines or Wire Erosion Machines.

II.A2.018 Computer controlled or “numerically controlled” co-ordinate measuring 2B006.a machines (CMM), or dimensional inspection machines, having a three dimensional (volumetric) maximum permissible error of indication 2B206.a (MPP E) at any point in the operating range of the machine (i.e. within the length axes) equal to or less (better) than (3 + L/1 000) μm (L is the measured length in mm), tested according to ISO 10360-2 (2001), and measurement probes designed therefor.

II.A2.019 Computer controlled or “numerically controlled” Electron Beam Welding 2B001.e.1.b Machines, and specially designed components therefor.

II.A2.020 Computer controlled or “numerically controlled” Laser Welding and Laser 2B001.e.1.c Cutting Machines, and specially designed components therefor.

II.A2.021 Computer controlled or “numerically controlled” Plasma Cutting 2B001.e.1 Machines, and specially designed components therefor.

II.A2.022 Vibration Monitoring Equipment specially designed for rotors or rotating 2B116 equipment and machinery, capable of measuring any frequency in the range 600-2 000 Hz.

II.A2.023 Liquid Ring Vacuum Pumps, and specially designed components 2B231 therefore. 2B350.i

II.A2.024 Rotary Vane Vacuum Pumps, and specially designed components 2B231 therefore. 2B235.i Note 1: II.A2.024 does not control rotary vane vacuum pumps that are specially designed for specific other equipment. 0B002.f 02012R0267 — EN — 18.01.2017 — 022.003 — 152

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Note 2: The control status of rotary vane vacuum pumps that are specially designed for specific other equipment is determined by the control status of the other equipment

II.A2.025 Air filters, as follows, having one or more physical size dimension 2B352.d exceeding 1 000 mm: (a) High Efficiency Particulate Air (HEPA) filters; (b) Ultra-Low Penetration Air (ULPA) filters. Note: II.A2.025 does not control air filters specially designed for medical equipment.

A3. Electronics

Related item from Annex I to No Description Regulation (EC) No 428/2009

II.A3.001 High voltage direct current power supplies having both of the following 3A227 characteristics: a. Capable of continuously producing, over a time period of eight hours, 10 kV or more, with output power of 5 kW or more with or without sweeping; and b. Current or voltage stability better than 0,1 % over a time period of four hours. Note: This item does not cover power supplies defined in items 0B001.j.5 and 3A227.

II.A3.002 Mass spectrometers, other than those specified in 3A233 or 0B002.g, 3A233 capable of measuring ions of 200 atomic mass units or more and having a resolution of better than 2 parts in 200, as follows, and ion sources thereof: a. Inductively coupled plasma mass spectrometers (ICP/MS); b. Glow discharge mass spectrometers (GDMS); c. Thermal ionisation mass spectrometers (TIMS); d. Electron bombardment mass spectrometers which have a source chamber constructed from, lined with or plated with ‘materials resistant to corrosion by uranium hexafluoride UF 6 ’; e. Molecular beam mass spectrometers having either of the following characteristics: 1. A source chamber constructed from, lined with or plated with stainless steel or molybdenum and equipped with a cold trap capable of cooling to 193 K (– 80 °C) or less; or 2. A source chamber constructed from, lined with or plated with ‘materials resistant to corrosion by uranium hexafluoride (UF6 )’; f. Mass spectrometers equipped with a microfluorination ion source designed for actinides or actinide fluorides. 02012R0267 — EN — 18.01.2017 — 022.003 — 153

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II.A3.003 Spectrometers and diffractometers, designed for the indicative test or — quantitative analysis of the elemental composition of metals or alloys without chemical decomposition of the material.

II.A3.004 Frequency changers or generators, and Variable Speed electrical drives, 3A225 other than those prohibited by 0B001 or 3A225, having all of the following characteristics, and specially designed components and 0B001.b.13 software therefor: a. Multiphase output capable of providing a power of 10 W or greater; b. Capable of operating at a frequency of 600 Hz or more; and c. Frequency control better (less) than 0,2 %. Technical Note: Frequency changers are also known as converters or inverters. Notes: 1. Item II.A3.004 does not control frequency changers that include communication protocols or interfaces designed for specific industrial machinery (such as machine tools, spinning machines, printed circuit board machines) so that the frequency changers cannot be used for other purposes while meeting the performance characteristics above. 2. Item II.A3.004 does not control frequency changers specially designed for vehicles and which operate with a control sequence that is mutually communicated between the frequency changer and the vehicle control unit.

A6. Sensors and Lasers

Related item from Annex I to No Description Regulation (EC) No 428/2009

II.A6.001 Yttrium aluminium garnet (YAG) rods —

II.A6.002 Optical equipment and components, other than those specified in 6A002, 6A002 6A004.b as follows: 6A004.b Infrared optics in the wavelength range 9 000 nm – 17 000 nm and components thereof, including cadmium telluride (CdTe) components.

II.A6.003 Wave front corrector systems for use with a laser beam having a diameter 6A003 exceeding 4 mm, and specially designed components thereof, including control systems, phase front sensors and ‘deformable mirrors’ including bimorph mirrors. Note: This item does not cover mirrors defined in 6A004.a, 6A005.e and 6A005.f. 02012R0267 — EN — 18.01.2017 — 022.003 — 154

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II.A6.004 Argon ion “lasers” having an average output power equal to or greater 6A005.a.6 than 5 W. 6A205.a Note: This item does not cover argon ion ‘lasers’ defined in items 0B001.g.5, 6A005 and 6A205.a.

II.A6.005 Semiconductor “lasers” and components thereof, as follows: 6A005.b a. Individual semiconductor “lasers” with an output power greater than 200 mW each, in quantities larger than 100; b. Semiconductor “laser” arrays having an output power greater than 20 W. Notes: 1. Semiconductor “lasers” are commonly called “laser” diodes. 2. This item does not cover “lasers” defined in items 0B001.g.5, 0B001.h.6 and 6A005.b. 3. This item does not cover “laser” diodes with a wavelength in the range 1 200 nm – 2 000 nm.

II.A6.006 Tunable semiconductor “lasers” and tunable semiconductor ‘laser’ arrays, 6A005.b of a wavelength between 9 μm and 17 μm, as well as array stacks of semiconductor ‘lasers’ containing at least one tunable semiconductor ‘laser’ array of such wavelength. Notes: 1. Semiconductor “lasers” are commonly called “laser” diodes. 2. This item does not cover semiconductor “lasers” defined in items 0B001.h.6 and 6A005.b

II.A6.007 Solid state “tunable” “lasers” and specially designed components thereof 6A005.c.1 as follows: a. Titanium-sapphire lasers, b. Alexandrite lasers. Note: This item does not cover titanium-sapphire and alexandrite lasers defined in items 0B001.g.5, 0B001.h.6 and 6A005.c.1.

II.A6.008 Neodymium-doped (other than glass) “lasers”, having an output wave 6A005.c.2 length greater than 1 000 nm but not exceeding 1 100 nm and output energy exceeding 10 J per pulse. Note: This item does not cover neodymium-doped (other than glass) ‘lasers’ defined in item 6A005.c.2.b.

II.A6.009 Components of acousto-optics, as follows: 6A203.b.4.c a. Framing tubes and solid-state imaging devices having a recurrence frequency equal to or exceeding 1 kHz; b. Recurrence frequency supplies; c. Pockels cells. 02012R0267 — EN — 18.01.2017 — 022.003 — 155

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II.A6.010 Radiation-hardened cameras, or lenses thereof, other than those specified 6A203.c in 6A203.c., specially designed, or rated as radiation-hardened, to 3 withstand a total radiation dose greater than 50 × 10 Gy (silicon) (5 × 6 10 rad (silicon)) without operational degradation. Technical Note: The term Gy(silicon) refers to the energy in Joules per kilogram absorbed by an unshielded silicon sample when exposed to ionising radiation.

II.A6.011 Tunable pulsed dye laser amplifiers and oscillators, having all of the 6A205.c following characteristics: 1. Operating at wavelengths between 300 nm and 800 nm; 2. An average output power greater than 10 W but not exceeding 30 W; 3. A repetition rate greater than 1 kHz; and 4. Pulse width less than 100 ns. Notes: 1. This item does not cover single mode oscillators. 2. This item does not cover tunable pulsed dye laser amplifiers and oscil lators defined in item 6A205.c, 0B001.g.5 and 6A005.

II.A6.012 Pulsed carbon dioxide “lasers” having all of the following characteristics: 6A205.d 1. Operating at wavelengths between 9 000 nm and 11 000 nm; 2. A repetition rate greater than 250 Hz; 3. An average output power greater than 100 W but not exceeding 500 W; and 4. Pulse width less than 200 ns. Note: This item does not cover pulsed carbon dioxide laser amplifiers and oscillators defined in item 6A205.d., 0B001.h.6. and 6A005.d.

II.A6.013 Copper vapour ‘lasers’ having both of the following characteristics: 6A005.b 1. Operating at wavelengths between 500 and 600 nm; and 2. An average output power equal to or greater than 15 W.

II.A6.014 Pulsed carbon monoxide ‘lasers’ having all of the following character istics: 1. Operating at wavelengths between 5 000 and 6 000 nm; 2. A repetition rate greater than 250 Hz; 3. An average output power greater than 100 W; and 4. Pulse width of less than 200 ns. Note: This item does not control the higher power (typically 1 to 5 kW) industrial carbon monoxide lasers used in applications such as cutting and welding, as these latter lasers are either continuous wave or are pulsed with a pulse width greater than 200 ns. 02012R0267 — EN — 18.01.2017 — 022.003 — 156

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II.A6.015 ‘Vacuum pressure gauges’, being electrically powered and having 0B001.b measurement accuracy of 5 % or less (better). ‘Vacuum pressure gauges’ include Pirani Gauges, Penning Gauges and Capacitance Manometers.

II.A6.016 Microscopes and related equipment and detectors, as follows: 6B (a) Scanning Electron Microscopes; (b) Scanning Auger Microscopes; (c) Transmission Electron Microscopes; (d) Atomic Force Microscopes; (e) Scanning Force Microscopes; (f) Equipment and detectors, specially designed for use with the micro scopes specified in II.A6.013 a) to e) above, employing any of the following materials analysis techniques: 1. X-ray Photo Spectroscopy (XPS); 2. Energy-dispersive X-ray Spectroscopy (EDX, EDS); or 3. Electron Spectroscopy for Chemical Analysis (ESCA).

A7. Navigation and Avionics

Related item from Annex I to No Description Regulation (EC) No 428/2009

II.A7.001 Inertial navigation systems and specially designed components thereof, as 7A003 follows: I. Inertial navigation systems which are certified for use on “civil 7A103 aircraft” by civil authorities of a State participating in the Wassenaar Arrangement, and specially designed components thereof, as follows: a. Inertial navigation systems (INS) (gimballed or strapdown) and inertial equipment designed for “aircraft”, land vehicle, vessels (surface or underwater) or ‘spacecraft’ for attitude, guidance or control, having any of the following characteristics, and specially designed components thereof: 1. Navigation error (free inertial) subsequent to normal alignment of 0,8 nautical mile per hour (nm/hr) ‘Circular Error Probable’ (CEP) or less (better); or 2. Specified to function at linear acceleration levels exceeding 10 g; b. Hybrid Inertial Navigation Systems embedded with Global Navi gation Satellite Systems(s) (GNSS) or with “Data-Based Referenced Navigation” (“DBRN”) System(s) for attitude, guidance or control, subsequent to normal alignment, having an INS navigation position accuracy, after loss of GNSS or “DBRN” for a period of up to four minutes, of less (better) than 10 metres ‘Circular Error Probable’ (CEP); 02012R0267 — EN — 18.01.2017 — 022.003 — 157

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Related item from Annex I to No Description Regulation (EC) No 428/2009

c. Inertial Equipment for Azimuth, Heading, or North Pointing having any of the following characteristics, and specially designed components thereof:

1. Designed to have an Azimuth, Heading, or North Pointing accuracy equal to, or less (better) than 6 arc/ minutes RMS at 45 degrees latitude; or

2. Designed to have a non-operating shock level of at least 900 g at a duration of at least 1 msec.

Note: The parameters of I.a. and I.b. are applicable with any of the following environmental conditions:

1. Input random vibration with an overall magnitude of 7,7 g rms in the first half hour and a total test duration of one and a half hours per axis in each of the three perpendicular axes, when the random vibration meets the following:

a. A constant power spectral density (PSD) value of 2 0,04 g /Hz over a frequency interval of 15 to 1 000 Hz; and

2 b. The PSD attenuates with a frequency from 0,04 g /Hz to 2 0,01 g /Hz over a frequency interval from 1 000 to 2 000 Hz;

2. A roll and yaw rate equal to or greater than + 2,62 radian/s (150 deg/s); or

3. According to national standards equivalent to 1. or 2. above.

Technical Notes:

1. I.b. refers to systems in which an INS and other independent navigation aids are built into a single unit (embedded) in order to achieve improved performance.

2. ‘Circular Error Probable’ (CEP) — In a circular normal distribution, the radius of the circle containing 50 percent of the individual measurements being made, or the radius of the circle within which there is a 50 percent probability of being located.

II. Theodolite systems incorporating inertial equipment specially designed for civil surveying purposes and designed to have an Azimuth, Heading, or North Pointing accuracy equal to, or less (better) than 6 arc minutes RMS at 45 degrees latitude, and specially designed components thereof.

III. Inertial or other equipment using accelerometers specified in 7A001 or 7A101, where such accelerometers are specially designed and developed as MWD (Measurement While Drilling) sensors for use in downhole well services operations.

II.A7.002 Accelerometers containing piezoelectric ceramic transducer element, 7A001 having a sensitivity of 1 000 mV/g or better (higher) 02012R0267 — EN — 18.01.2017 — 022.003 — 158

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A9. Aerospace and Propulsion

Related item from Annex I to No Description Regulation (EC) No 428/2009

II.A9.001 Explosive bolts. —

II.A9.002 ‘Load Cells’ capable of measuring rocket motor thrust having a capacity 9B117 exceeding 30 kN. Technical Note: ‘Load Cells’ means devices and transducers for the measurement of force in both tension and in compression. Note: II.A9.002 does not include equipment, devices or transducers, specially designed for the measurement of the weight of vehicles, e.g. weigh bridges.

II.A9.003 Electrical power generation gas turbines, components and related 9A001 equipment as follows: 9A002 (a) Gas Turbines specially designed for electrical power generation, 9A003 having an output exceeding 200 MW; 9B001 (b) Vanes, Stators, Combustion Chambers and Fuel Injection Nozzles, specially designed for electrical power generation gas turbines 9B003 specified in II.A9.003.a; 9B004 (c) Equipment specially designed for the “development” and “production” of electrical power generation gas turbines specified in II. A9.003.a.

II.B. TECHNOLOGY

Related item from Annex I to No Description Regulation (EC) No 428/2009

II.B.001 Technology required for the development, production, or use of the items — in Part II.A. (Goods) above.

Technical Note: The term ‘technology’ includes software. 02012R0267 — EN — 18.01.2017 — 022.003 — 159

use in the systems specified in 1.A., 19.A.1. use in the systems specified or 19.A.2. and the subsystems specified in 2.A. or 20.A. Missile Technology Control Regime (M.TCR): Equipment, software and technology annex

M6A1 Composite structures, laminates, and manufactures thereof, specially designed for designed specially thereof, manufactures and laminates, structures, M6A1 Composite ANNEX III or m;

4 and m;

6 and CATEGORY 1 — SPECIAL MATERIALS AND RELATED EQUIPMENT MATERIALSAND SPECIAL — CATEGORY 1 ;

of dual-use items or b. A length not exceeding 2,5 m; 2,5 exceeding not length b. A c. A width exceeding 15 mm. 15 exceeding width c. A civilian applications as follows: goods; a. Sporting industry; b. Automotive industry; tool c. Machine applications. d. Medical epoxy resin impregnated carbon materials” for “fibrous or filamentary aircraft” structures or the laminates, repair of “civil having all of the following: m 1 exceeding not area a. An b. A “specific tensile strength” exceeding 17,7 × 10 × 17,7 exceeding strength” tensile “specific b. A a. A “specific modulus” exceeding 10,15 × 10 × 10,15 exceeding modulus” “specific a. A or 1C010.e.; 2. Materials specified in 1C010.c. in specified 2. Materials 1. having of the following: all materials” Carbon or filamentary “fibrous a. Consisting of an organic “matrix” and materials specified in 1C010.c., 1C010.d. 1C010.c., in specified materials and “matrix” organic an of a. Consisting b. Consisting and or carbon “matrix”, any of the following: of a metal Note 1: 1A002 does not control composite structures or laminates made from purely for designed specially items, semi-finished control Note 2: not does 1A002 1A002 having any or laminates, “Composite”following: of the structures The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/ Council Regulation (EC) in identified corresponding equipment and components as systems, The 2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit and brokering transfer, exports, of control the for Community regime a 5 up setting 2009 of 2009 May 1A Systems, Equipment and Components and Equipment 1A Systems, M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 160

following: a. Designed for rocket systems; and following: a. Designed rocket systems; b. for Usable in the systems specified in 1.A. or 19.A.1. the manu axes, designed for or more and programmed in two be co-ordinated facture of and composite airframes missile structures; motions for positioning, wrapping and winding fibres can be coordinated and be coordinated can positioning, wrapping and winding fibres motions for composite structures more axes, designed to fabricate or programmed in three and co-ordinating and materials, filamentary fibrous or from or laminates programming controls Missile Technology Control Regime (M.TCR): Equipment, software and technology annex M6A2 Resaturated pyrolised (i.e. carbon-carbon) components having all of the of all having components carbon-carbon) (i.e. pyrolised M6A2 Resaturated M6B1a Filament winding machines or ‘fibre/tow-placement machines’, of which the which of machines’, ‘fibre/tow-placement or machines winding M6B1a Filament M6B1b ‘Tape-laying machines’ of which the motions for positioning and laying tape can tape laying and positioning for motions the which of machines’ M6B1b ‘Tape-laying

of dual-use items

application. two dimensions of interwovenfilaments and speciallydesigned for applications as follows: metals; tempering for furnaces heat-treatment a. Metal equipment. production boule b. Silicon are coordinated and programmed in five servo or more ‘primary positioning’ or “composite” airframe of the manufacture designed for specially axes, structures; ‘missile’ and winding fibres are coordinated and programmed in three or more ‘primary more or in three and programmed coordinated are and winding fibres of “composite” servo positioning’designed the manufacture axes, specially for materials”; or filamentary from “fibrous or laminates, structures Note 4: 1A002 does not control finished items specially designed for a specific vehicles specified in 9A004 or sounding rockets specified in 9A104. tape laying and positioning for motions the which of machines’, b. ‘Tape-laying a. positioning, wrapping motions for winding which the machines, of Filament Note 3: 1A002.b.1. does not control items containing semi-finished a maximum of specified in 1A002 or “fibrous or filamentary materials” specified in 1C010, specified as materials” in 1A002 specified or filamentary or “fibrous therefor: designed components and accessories follows, and specially 1B201. AND 1B101 ALSO N.B.: SEE 1B001 Equipment or laminates for the production structures or inspection of “composite” 1A102 Resaturated pyrolized carbon-carbon components designed for space launch space for designed components carbon-carbon pyrolized 1A102 Resaturated The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/ Council Regulation (EC) in identified corresponding equipment and components as systems, The 2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit and brokering transfer, exports, of control the for Community regime a 5 up setting 2009 of 2009 May Equipment Production and Inspection 1B Test, M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 161

resinimpregnated tape, tow, or fibre. Fully or partially resin-impregnated or partially Fully tow, or fibre. resinimpregnated tape, ‘filament bands’ include those coated with dry powder that tacks upon heating. chines that perform similar processes that use computer-guided heads to a part or bands’onto a mold to create ‘filament lay one or several structure. These machines have the ability to cut and restart individual ‘filament band’ courses during the laying process. ‘filament bands’ having widths less than or equal to 25,4 mm. This refers to the minimum width the machine of material can place, regardless of the upper capability of the machine. bands’mm, having but widths cannot less than place or equal to 304,8 refers mm. This than 25,4 less or a width equal to bands’with ‘filaments to the minimum width the machine of material can place, regardless of the upper capability of the machine. 1. A ‘filament band’ is a single continuous width of fully or partially ‘Fibre/tow-placement machines’ and ‘tape-laying 2. machines’ are ma- more or one place to ability the have machines’ 3. ‘Fibre/tow-placement ‘filament more or one place to ability the have machines’ 4. ‘Tape-laying stated. polycarbosilane) including provision special the during to strain fibre heating; including adapters and modification kits for weaving, interlacing or braiding or weaving, interlacing for kits and modification including adapters fibres to manufacture composite structures; Note: For the purposes of 6.B.1.a. and 6.B.1.b., apply: the following definitions Note: 6.B.1.c. does not control textile machinery not modified for the end-uses the for modified not machinery textile control not does Note: 6.B.1.c. Equipment designed or modified for the production of fibrous or filamentary materials as follows: M6B1c Multi-directional, multi-dimensional weaving machines or interlacing machines, interlacing or machines weaving multi-dimensional M6B1c Multi-directional, M6B1d1 1. Equipment for converting polymeric fibres (such as polyacrylonitrile, rayon, or rayon, polyacrylonitrile, as (such fibres polymeric converting for Equipment M6B1d1 1.

aerial vehicle systems. aerial vehicle pitch or polycarbosilane) into carbon fibres or silicon carbide fibres, or silicon carbide or polycarbosilane) into carbon pitch fibres during heating; fibre the strain equipment to including special Technical Note: For the purposes of 1B001.b., one to lay have ability machines’the ‘tape-laying mm and than or to widths less than bands’greater 25 limited or more ‘filament band’courses individual ‘filament and mm, and to cut restart 305 equal to process. laying during the Note: In 1B001.b., ‘missile’ means complete rocket systems and unmanned and systems rocket complete means ‘missile’ 1B001.b., Note: In Technical Note: For the purposes 1B001.c., of includes knitting. the technique of interlacing 1. Equipment for converting polymeric fibres (such as polyacrylonitrile, rayon, polyacrylonitrile, as (such fibres polymeric converting for 1. Equipment including adapters and modification kits, specially designed for or modified specially kits, and including adapters modification structures; “composite” for fibres, braiding or weaving, interlacing fibres, as follows: c. Multidirectional, multidimensional weaving machines or interlacing machines, interlacing or machines weaving multidimensional c. Multidirectional, d. Equipment designed specially or adapted for the production of reinforcement

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6.B.1. are moulds, mandrels, dies, fixtures and tooling for the preform the for tooling and fixtures dies, moulds, mandrels, 6.B.1. are structures, bonding composite or of sintering pressing, curing, casting, laminates and manufactures thereof filament substrates; oxide) producing prepregs and preforms, including rollers, tension stretchers, coating stretchers, tension rollers, including preforms, and producing prepregs dies. and clicker equipment equipment, cutting Note: Examples of components and accessories for the machines specified in M6B1e Equipment designed or modified for special fibre surface treatment or for or treatment surface fibre special for modified or designed M6B1e Equipment M6B1d2 2. vapour Equipment for the or compounds deposition of elements on heated M6B1d3 3. (such as aluminium ceramics the wet-spinning Equipment of refractory for

on heated filamentary substrates, to manufacture silicon carbide fibres; carbide silicon manufacture to substrates, filamentary on heated oxide); by heat treatment; alumina fibres computer program direction, the position of the end effector (i.e., head) computer program in (i.e., the position the end of effector direction, correct orientation and at the to the work to piece direction space relative achieve the desired process. or partially resin-impregnated tape, tow fibre. of fully positioning transmitters or receivers are simultaneously coordinated and simultaneously coordinated are or receivers positioning transmitters dimensional the three or more axes to follow programmed in four component the under inspection; contours of Technical Note: purposes 1B001.g., For the of to have the ability ‘tow-placement machines’ place one bands’or more ‘filament having mm, widths less than or equal to 25 placement during the band’courses individual ‘filament and restart cut and to process. Technical Note: under control, axes positioning’ servo ‘primary 1B001, of purpose the 1. For 2. the purposes For of 1B001., continuous band’a single is a ‘filament width method; materials, as follows: inspection; defect dimensional three for for systems motions tomography 1. X-ray the which of machines testing ultrasonic controlled 2. Numerically coordinated and tows are servo posi programmed in two or more ‘primary tioning’ axes, specially designed for the of manufacture “composite” airframe structures. or ‘missile’ 2. vapour Equipment deposition the or compounds, chemical for of elements 3. (such as aluminium ceramics Equipment the wet-spinning for of refractory 4. Equipment for converting aluminium containing precursor fibres into e. Equipment for producing prepregs specified in 1C010.e. by the hot melt hot the by 1C010.e. in specified prepregs producing for e. Equipment “composite” for designed specially equipment inspection f. Non-destructive laying and positioning for motions the which of machines’, g. ‘Tow-placement

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propellants constituents specified in 4.C., propellants constituents specified in and energy specified fluid mills 4.B.3. in specified those 4.B., are with 4.B.2. be evaluated in accordance motions for positioning, wrapping and winding fibres can be coordinated and be coordinated can positioning, wrapping and winding fibres motions for composite structures more axes, designed to fabricate or programmed in three and co-ordinating and materials, filamentary fibrous or from or laminates programming controls; environment, of spherical, spheroidal or atomised materials specified in 4.C.2.c., specified materials atomised or spheroidal spherical, environment, of frequency (high generators Plasma a. includes: 4.B.3.d. Note: 4.C.2.e. 4.C.2.d. or arc-jet) usable for obtaining sputtered or spherical metallic powders with organ ization of the process in equipment environment; b. an argon-water Electroburst powders of with organization metallic or spherical obtaining sputtered usable for the “pro environment; c. Equipment usable for the process in an argon-water aluminium powders duction”by of spherical powdering in an inert a melt medium (e.g. nitrogen). Notes: or propellants solid continuous usable for The only batch mixers, mixers, 1. to are 4.B.3.d. in specified not equipment” “production powder metal of 2. Forms M6B1a Filament winding machines or ‘fibre/tow-placement machines’, of which the which of machines’, ‘fibre/tow-placement or machines winding M6B1a Filament M4B3d Metal powder “production equipment” usable for the “production”, in a controlled a in “production”, the for usable equipment” “production powder M4B3d Metal

dies, fixtures and tooling for the preform pressing, curing, casting, sintering pressing, curing, casting, sintering preform the and tooling for dies, fixtures or bonding thereof. and manufactures laminates of composite structures, for positioning, wrapping and winding can be coordinated and fibres composite structures axes, designed to fabricate more or programmed in three and coordinating and materials, filamentary or fibrous from or laminates programming controls; a. Filament winding machines or fibre placement machines, of which the motions the which of machines, placement fibre or machines winding a. Filament specially designed to avoid contamination and specially designed for use in one of in 1C002.c.2. the processes specified 1B102. ALSO N.B.: SEE composites as follows; and specially designed components and accessories and specially follows; as composites therefor: 1B201. ALSO N.B.: SEE mandrels, moulds, include 1B101 in specified accessories and Note: Components 1B002 Equipment for producing metal alloys, metal alloy powder or alloyed materials, 1B101 Equipment, other than that specified in 1B001, for the “production” of structural of “production” the for 1B001, in specified that than other 1B101 Equipment,

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polycarbosilane) including special provision to strain the fibre during heating; the fibre provision polycarbosilane) including to strain special filament substrates; oxide); pregnated tape, tow, or fibre. Fully or partially resin-impregnated ‘filament ‘filament resin-impregnated partially or Fully fibre. or tow, pregnated tape, bands’ include those coated with dry powder that tacks upon heating. one or use computer-guided lay heads to processes that perform similar a structure. These a part or bands’onto a mold to create ‘filament several band’courses ‘filament individual and restart cut to ability machines have the process. laying during the ‘filament bands’mm. having This refers to widths less than or equal to 25,4 upper the of machine can place, regardless material the minimum width of the capability of the machine. ‘filaments cannot place but mm, 304,8 to equal than or less having widths bands’ with a width equal mm. to or less than This refers to the minimum 25,4 width the machine of material can place, regardless of the upper capability of the machine. 1. Equipment for converting polymeric fibres (such as polyacrylonitrile, rayon, or rayon, materials as follows: polyacrylonitrile, as (such fibres polymeric converting for 1. Equipment compounds or vapour the deposition of elements on 2. Equipment heated for (such as aluminium ceramics 3. Equipment for the wet-spinning of refractory Note: purposes 6.B.1.a. of For the and apply: 6.B.1.b., following definitions the resinim partially or fully of width continuous single a is band’ ‘filament 1. A 2. ‘Fibre/tow-placement machines’ and ‘tape-laying machines’ are machines that 3. ‘Fibre/tow-placement machines’ have the ability to place one or more 4. bands’ to place one or more ‘filament have the ability ‘Tape-laying machines’ be co-ordinated and programmed in two or more axes, designed for the manu axes, designed for or more and programmed in two be co-ordinated facture of and composite airframes missile structures; M6B1d Equipment designed or modified for the production of fibrous or filamentary M6B1b ‘Tape-laying machines’ of which the motions for positioning and laying tape can tape laying and positioning for motions the which of machines’ M6B1b ‘Tape-laying or polycarbosilane) including special provision to strain the fibre during fibre the provision strain to including special or polycarbosilane) heating; filament substrates; oxide); materials” as follows: materials” rayon polyacrylonitrile, as (such fibres polymeric converting for 1. Equipment 2. Equipment for the vapour deposition or compounds of elements on heated aluminium as (such ceramics refractory of wet-spinning the for 3. Equipment sheets can be coordinated and programmed in two or more axes, designed for can be coordinated and programmed in two or more sheets structures; and “missile” of composite airframe the manufacture c. or filamentary “production”of “fibrous the Equipment modified for designed or b. and positioning and laying tape motions for which the of Tape-laying machines

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sputtered or spherical metallic powders sputtered or spherical metallic with organization of the an process in argon-water environment; metallic powders with organization of the process in an argon-water environment; by powdering in an inert medium a melt (e.g. nitrogen). 6.B.1. are moulds, mandrels, dies, fixtures and tooling for the preform the for tooling and fixtures dies, moulds, mandrels, 6.B.1. are structures, bonding composite or of sintering pressing, curing, casting, laminates and manufactures thereof a. Plasma generators (high frequency arc-jet) usable for obtaining b. Electroburst equipment usable for obtaining sputtered or spherical c. Equipment usable for the “production” of spherical aluminium powders propellants constituents specified in 4.C., and fluid energy mills specified in specified 4.C., energy mills and in fluid specified propellants constituents in 4.B.3. specified those 4.B., are to be evaluated in accordance with 4.B.2. Note: Examples of components and accessories for the machines specified in environment, of spherical, spheroidal or atomised materials specified in 4.C.2.c., specified materials atomised or spheroidal spherical, environment, of 4.C.2.e. 4.C.2.d. or producing prepregs and preforms, including rollers, tension stretchers, coating stretchers, tension rollers, including preforms, and producing prepregs dies. and clicker equipment equipment, cutting Notes: The only batch mixers, continuous 1. mixers, usable for solid propellants or 2. powder Forms of metal in 4.B.3.d. “production are equipment”not specified Note: 4.B.3.d. includes: Note: 4.B.3.d. M6B1e Equipment designed or modified for special fibre surface treatment or for or treatment surface fibre special for modified or designed M6B1e Equipment M4B3d Metal powder “production equipment” usable for the “production”, in a controlled a in “production”, the for usable equipment” “production powder M4B3d Metal

sputtered or spherical metallic powders sputtered or spherical metallic with organization of the an argon-water process in environment; powders metallic with organization of the process in an argon-water environment; nitrogen). (e.g. medium an inert in powders by powdering melt a a. Plasma generators (high frequency arc-jet) usable for obtaining spherical or sputtered obtaining for usable equipment b. Electroburst c. Equipment usable for the “production” of spherical aluminium equipment and clicker dies. equipment and clicker producing prepregs and preforms specified in entry 9C110. entry in specified preforms and producing prepregs spheroidal or atomised materials controlled environment, of spherical, in 1C011.a.,specified 1C011.b., 1C111.a.1., 1C111.a.2. the Military in or Goods Controls. or 1B102.a. Note: 1B101.d. includes rollers, tension stretchers, coating equipment, cutting equipment, coating stretchers, tension rollers, includes Note: 1B101.d. includes: Note: 1B102 d. Equipment designed or modified for special fibre surface treatment or for treatment surface Equipment fibre designed special or modified for d. follows: components as 1B115.b. ALSO N.B.: SEE a. Metal powder “production equipment” usable for the “production”, in a 1B002 in specified equipment” “production for components designed b. Specially 1B102 Metal powder “production equipment”, other than that specified in 1B002, and 1B002, in specified that than other equipment”, “production powder 1B102 Metal

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deagglomerators or knife-spindles. deagglomerators or Note: In Item 4.B.3.a.2. the term ‘mixing/kneading shaft’ does not refer to refer not does shaft’ ‘mixing/kneading term the 4.B.3.a.2. Item Note: In “production”, handling or acceptance testing of liquid propellants or propellant or of liquid propellants “production”, testing handling or acceptance in 4.C. constituents specified designed components therefor, for the production, handling, mixing, curing, production, handling, mixing, the for designed components therefor, casting, pressing, machining, testing of solid propellants extruding or acceptance in 4.C. or propellant constituents specified 13,326 kPa and with temperature control capability of the mixing chamber and mixing chamber the of capability control 13,326 kPa and with temperature following: the of having all 1. or more; and of 110 capacity A volumetric litres total centre; off mounted shaft’ ‘mixing/kneading one least 2. At M4B1 “Production equipment”, and specially designed components therefor, for the for therefor, components designed specially and equipment”, M4B1 “Production M6B2 to in 6.E.3. processes referred designed the for Nozzles specially M4B2 “Production equipment”, other than that described in 4.B.3., and specially and 4.B.3., in described that than other equipment”, M4B2 “Production M4B3a Batch mixers with provision for mixing under vacuum in the range of zero to zero of range the in vacuum under mixing for provision with mixers M4B3a Batch

and

see the Military Goods see the Military Controls. acceptance testing of boron carbide. acceptance testing lomerators or knife-spindles. energy mills. For the control of batch mixers, continuous and of batch mixers, For the control mixers energy mills. see 1B117, fluid energy mills 1B118 and 1B119. pressing, testing of solid propellants or machining, extruding or acceptance propellant constituents specified in 1C011.a., 1C011.b., 1C111 or in the Military Goods Controls. liquid propellants or propellant constituents specified in 1C011.a., or propellant constituents specified liquid propellants 1C011.b., Controls; Goods Military the in 1C111 or goods, military of production the for designed specially Note 1: equipment For Note: 1B115.b. does not control batch mixers, continuous mixers or fluid Note 2: 1B115 “production”,the does not control equipment for handling and Note: In 1B117.b. the term ‘mixing/kneading shaft’ does not refer to deagg to refer not does shaft’ ‘mixing/kneading term the 1B117.b. Note: In b. “Production equipment” for the “production”, handling, mixing, curing, casting, curing, mixing, handling, “production”, the for equipment” b. “Production a. “Production equipment” for the “production”, handling or acceptance testing of testing acceptance or handling “production”, the for equipment” a. “Production a mould, mandrel or other substrate from precursor gases which decompose precursor from in the a mould, other substrate or mandrel 130 Pa of pressures at range temperature °C) 900 (2 173 K 3 to °C) 300 (1 573 K 1 to 20 kPa. centre. off mounted shaft’ ‘mixing/kneading one least b. At propellant and propellant constituents, as follows, and designed propellant and constituents, as specially propellant components therefor: 13,326 kPa and with temperature control capability of the mixing chamber and 13,326 control capability kPa and with temperature components therefor: designed and specially following, the of having all a. or more; of 110 capacity volumetric A litres total 1B116 Specially designed nozzles for producing pyrolitically derived materials formed on formed materials derived pyrolitically producing for nozzles designed 1B116 Specially 1B115 Equipment, other than that specified in 1B002 or 1B102, for the production of production the for 1B102, or 1B002 in specified that than other 1B115 Equipment, 1B117 Batch mixers with provision for mixing under vacuum in the range of zero to zero of range the in vacuum under mixing for provision with mixers 1B117 Batch

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shaft as well as inside the casing of mixing chamber; shaft as well designed for reduced or tailored reflectivity or emissivity in the microwave, in or emissivity designed for reduced or tailored reflectivity spectra. infrared or ultraviolet thermal control of satellites. signatures and acoustic signatures (i.e. stealth technology), signatures and signatures (i.e. stealth acoustic for applications usable 1.A. in or 19.A. in 2.A. the systems specified subsystems for or the specified to 13,326 kPa and with a temperature control capability of the mixing chamber of control capability to 13,326 temperature kPa and with a following: the of having any or shafts; mixing/kneading more the or 1. Two on teeth/pins kneading having and oscillates which shaft rotating single 2. A Notes: specially paints), (including coatings and materials structural includes 1. 17.C.1. 2. used for 17.C.1. paints) when specially coatings (including does not control Missile Technology Control Regime (M.TCR): Equipment, software and technology annex M4B3c in 4.C substances specified grinding or milling usable for Fluid energy mills M17C1 Materials for reduced observables such as radar reflectivity, ultraviolet/infrared reflectivity, radar as such observables reduced for M17C1 Materials M4B3b Continuous mixers with provision for mixing under vacuum in the range of zero of range the in vacuum under mixing for provision with mixers M4B3b Continuous

Hz;

12 Hz but less than 3 Hz but less × 10

8 of dual-use items loading, or organic materials, including binders, providing including binders, materials, organic loading, or a bandwidthecho compared over % with metal more than 5 a. Plastic foam materials (flexible or non-flexible) with carbon- with non-flexible) or (flexible materials foam a. Plastic non-magnetic loading to provide absorption; non-magnetic loading provide to and convoluted wedges pyramids, cones, shape, including planar in surfaces; following: the of any from 1. Made a. Hair type absorbers, constructed of natural or synthetic fibres, with fibres, synthetic or natural of constructed absorbers, non- type a. Hair is surface incident whose and loss magnetic no having b. Absorbers following: the of all having absorbers, c. Planar Note 1: 1C001.a. control: does not shaft as well as inside the casing of the mixing chamber. as inside the casing of shaft as well

13,326 kPa and with a temperature control capability of the mixing chamber mixing the of capability control temperature a with and 13,326 kPa components therefor: designed and specially following, the of having any or shafts; mixing/kneading more or a. Two the on teeth/pins kneading having and oscillates which shaft rotating single b. A 1C011.b., 1C111 or in the Military Goods Controls, and specially designed specially and Controls, Goods Military the in or 1C011.b., 1C111 components therefor. intrinsically conductive polymers, as follows: 10 × 2 1C101. ALSO exceeding N.B.: SEE frequencies absorbing for a. Materials 1B118 Continuous mixers with provision for mixing under vacuum in the range of zero to zero of range the in vacuum under mixing for provision with mixers 1B118 Continuous 1B119 in 1C011.a., grinding or milling substances specified usable for Fluid energy mills 1C001 Materials specially designed for use as absorbers of electromagnetic waves, or waves, electromagnetic of absorbers as use for designed specially 1C001 Materials The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/ Council Regulation (EC) in identified corresponding equipment and components as systems, The 2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit and brokering transfer, exports, of control the for Community regime a 5 up setting 2009 of 2009 May 1C Materials M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 168

;

2 Hz but less than 3,7 × Hz but less than 3,7

14 N/m

and 6 ;

2 N/m

and or

or exceeding ± 15 exceeding % of the centre frequency of the incident energy, 450 K withstanding temperatures exceeding capable of and not (177 °C); with metal over a bandwidth exceeding ± 15 % of the centre with metal over a bandwidth ± 15 exceeding frequency of the incident energy, and not capable of withstanding temperatures exceeding 800 K (527 °C); Technical Note: square a 1C001.a. 1.c.1. should be for samples Note: Absorption test at least 5 wavelengths frequency on of the centre a side and posi radiating of the element. far field tioned in the b. Ceramic materials providing more than 20 % echo compared echo % 20 than more providing materials b. Ceramic A maximum operating temperature of 548 K (275 °C). A specific gravity exceeding 4,4; gravity exceeding A specific 2. 1. 3. Compressive strength less than 14 × 10 × 14 than less strength 3. Compressive 2. Tensile strength less than 7 × 10 × 7 than less strength 2. Tensile absorption when contained in paint. in contained absorption when d. Planar absorbers made of sintered ferrite, having all of the following: the of all having ferrite, sintered of made absorbers d. Planar b. Laser welding of polymers. of welding b. Laser any of the following applications: the any of polymers; of marking a. Laser Hz and not transparent to visible light; Hz and not transparent

14 exceeding 10 000 S/m (Siemens per metre) or a ‘sheet (surface) resistivity’ of resistivity’ (surface) ‘sheet a or metre) per (Siemens S/m 000 exceeding 10 less than 100 ohms/square, based on any of the following polymers: Note 2: Nothing Note in Note 1 to 1C001.a. 2: magnetic materials to provide releases 10 Note: 1C001.b. does not control materials, specially designed or formulated for formulated or designed specially materials, control not does Note: 1C001.b. c. Intrinsically conductive polymeric materials with a ‘bulk electrical conductivity’ electrical ‘bulk a with materials polymeric conductive c. Intrinsically b. Materials for absorbing frequencies exceeding 1,5 × 10 × 1,5 exceeding frequencies absorbing for b. Materials

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usable in systems specified in 1.A. specified or 19.A.1.; usable in systems composites usable for nose ceramic tips, Reinforced silicon-carbide re-entry in 1.A. 19.A.1. usable in systems specified or flaps, vehicles, nozzle a. Bulk machinable silicon-carbide reinforced unfired ceramic usable for nose tips nose for usable ceramic unfired reinforced silicon-carbide machinable a. Bulk from 100 MHz to 100 GHz) for use in missile radomes usable in systems use in missile GHz) for MHz to 100 from 100 specified in 1.A. or 19.A.1. M6C6 Silicon-carbide materials as follows: as materials M6C6 Silicon-carbide M6C5 Ceramic composite materials (dielectric constant less than 6 at any frequency any at 6 than less constant (dielectric materials composite M6C5 Ceramic

m and no more than 10 % of the particles % of the m and no than 10 more μ

or m; μ and a. Si-N; b. Si-C; c. Si-Al-O-N; d. Si-O-N; of borides of titanium with a density of 98 % or more of the theoretical density; of the theoretical % or more with a density of 98 of borides titanium reinforced with fibres having all of the following: materials: following the of any from 1. Made impurities, excluding intentional additions, of less than 5 000 ppm, an average 000 impurities, excluding intentional additions, of less than 5 particle size equal to or less than 5 larger than 10 2. Having a “specific tensile strength” exceeding 12,7 × 10 2. exceeding strength” 12,7 tensile Having a “specific 5. Poly thienylene-vinylene. 5. Poly Note: 1C007.b. does not control abrasives. control not does Note: 1C007.b. 1. Polyaniline; 2. Polypyrrole; form. 3. Polythiophene; liquid a phenylene-vinylene; 4. Poly in materials control not does Note: 1C001.c. Technical Note: should be and conductivity’ resistivity’ ‘sheet (surface) ‘Bulk electrical determined using ASTM D-257 or national equivalents. a. Ceramic powders of single or complex borides of titanium, having total metallic b. Non-“composite” ceramic materials in crude or semi-fabricated form, composed form, semi-fabricated or crude in materials ceramic b. Non-“composite” c. Ceramic-ceramic “composite” materials with a glass or oxide-“matrix” and with a glass or oxide-“matrix” “composite” materials Ceramic-ceramic c. posite” materials and precursor materials, as follows: materials, and precursor posite” materials 1C107. ALSO N.B.: SEE 1C007 Ceramic powders, non-“composite” ceramic materials, ceramic-“matrix” “com ceramic-“matrix” materials, ceramic non-“composite” powders, 1C007 Ceramic

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 170

4 and

(CAS 1344-28-1);

systems with a fibre tensile strength of less than 700 MPa at 1 273 K strength of less than 700 tensile with a MPa at 1 fibre systems creep strain % of more than 1 creep resistance tensile °C) or fibre 000 (1 hours. 100 for °C) 000 (1 K 273 and 1 load 100 MPa at O 2

components); Note: 1C007.f. does not control “composites” containing fibres from these 2. Si-C-N. 1. “Specific modulus” exceeding 12,7 × 10 × 12,7 exceeding modulus” 1. “Specific phase, incorporating particles, whiskers or fibres, where carbides or nitrides of nitrides or carbides where or fibres, whiskers particles, phase, incorporating silicon, zirconium or boron the “matrix”; form for producing any phase in 1C007.c., specified or phases of the materials as follows: carbide); silicon producing (for 1. Polydiorganosilanes nitride); silicon producing (for 2. Polysilazanes nitrogen and carbon silicon, with ceramics producing (for 3. Polycarbosilazanes reinforced with continuous fibres from any of the following systems: 1. Al polyethylene. control not does Note: 1C010.a. 2. “Specific tensile strength” exceeding 23,5 × 10 × 23,5 exceeding strength” tensile 2. “Specific N.B.: SEE ALSO 1C210 AND 9C110. AND 1C210 ALSO N.B.: SEE following: the of all having materials”, filamentary or “fibrous a. Organic d. without a continuous with or metallic “composite” materials, Ceramic-ceramic materials) metallo-organic or polymeric purpose special (i.e., materials e. Precursor Ceramic-ceramicf. “composite” materials with an oxideglass or “matrix” 1C010 follows: as materials”, filamentary “Fibrous or

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 171

4 and and

m; 6

6 and ;

structures or laminates, having all of the following: m 1 exceeding not area 1. An % by weight or more silica, or random fibre mat form, containing 3 10 × modulus”than with a “specific of less 10 or sublimation point lower than 2 043 K (1 770 °C) in an inert °C) 770 043 K (1 or sublimation point lower than 2 environment. 3. A width exceeding 15 mm. 15 exceeding width 3. A length. in mm or less materials” 25,0 2. A length not exceeding 2,5 m; 2,5 exceeding not length 2. A a. “Fibrous or filamentary materials”, for the repair of “civil aircraft” “civil of repair the for materials”, filamentary or a. “Fibrous chopped in fibres alumina polycrystalline multiphase, a. Discontinuous, b. Molybdenum and molybdenum alloy fibres; alloy molybdenum and b. Molybdenum fibres; c. Boron decomposition softening, melting, a with fibres ceramic d. Discontinuous b. Mechanically chopped, milled or cut carbon “fibrous or filamentary or “fibrous carbon cut or milled chopped, b. Mechanically (1 649 °C) in an inert environment; or specific weight of “fibrous or filamentary materials” in 1C010.a.,of “fibrous or filamentary weight 1C010.b. or specific or 1C010.c., strength the tensile and modulus should be determined by using ISO 10618 described in Method A (2004) or national equivalents. 1. “Specific modulus” exceeding 2,54 × 10 × 2,54 exceeding modulus” 1. “Specific 2. Melting, softening, decomposition or sublimation point exceeding 1 922 K 922 1 exceeding point sublimation or decomposition softening, 2. Melting, 1. “Specific modulus” exceeding 14,65 × 10 × 14,65 exceeding modulus” 1. “Specific 10 × 26,82 exceeding strength” tensile 2. “Specific control: not does Note: 1C010.b. control: not does Note: 1C010.c. Technical Notes: 1. For the purpose of calculating “specific tensile strength”, “specific modulus” c. Inorganic “fibrous or filamentary materials”, having all of the following: the of all having materials”, filamentary or “fibrous c. Inorganic b. having of the following: all materials”, Carbon or filamentary “fibrous

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divided by

, measured at a temperature of (296 ± , measured at a temperature of (296

3 , measured at a temperature of (296 ± 2)K ((23 ± ± 2)K ((23 , measured at a temperature of (296

3 using resins with a glass transition temperature (Tg), after cure, exceeding cure, after (Tg), a glass transition temperature with using resins °C as determined by ASTM D4065 or national equivalents. 145 2)°C) and a relative humidity of (50 ± 5)%. 2)°C) and humidity of (50 a relative 2)K ((23 ± 2)°C) and a relative humidity of (50 ± 5)%. ± 2)°C) and humidity a of (50 relative 2)K ((23 the specific weight in N/m the specific divided by the specific weight divided by in N/m the specific specified in 6.A.1., made either with organic matrix or metal matrix utilising strength greater tensile having a specific reinforcements fibrous or filamentary m. × 106 than 3,18 modulus m and greater a specific × 104 than 7,62 2. In Item 6.C.1. ‘specific modulus’ is the Young's modulus in N/m in modulus Young's the is modulus’ ‘specific 6.C.1. Item 2. In Note: The only resin impregnated fibre prepregs specified in 6.C.1. are those 6.C.1. are in specified prepregs fibre impregnated resin only Note: The Technical Notes: 1. In Item 6.C.1. ‘specific tensile strength’ is the ultimate tensile strength in N/m M6C1 Resin impregnated fibre prepregs and metal coated fibre preforms, for the goods or and m;

4 and m;

6 or or

equal to or exceeding 453 K (180 °C) and having a phenolic resin; or and having phenolic resin; °C) a or exceeding 453 equal to K (180 2. “Specific tensile strength” exceeding 17,7 × 10 2. strength” exceeding 17,7 tensile “Specific following: × 10 1. modulus” exceeding 10,15 “Specific weight of non-unidirectional “fibrous or filamentary materials” (e.g., fabrics, materials” (e.g., or filamentary weight of non-unidirectional “fibrous mechanical the on based be to 1C010. is in braids) or random mats unidirectional monofilaments constituent (e.g., monofila- properties of the non-unidirectional ments, yarns, to processing into the rovings or tows) prior materials”. “fibrous or filamentary a. Polyetherimides specified in 1C008.a.; in specified a. Polyetherimides b. Materials specified in 1C008.b. to 1C008.f.; to 1C008.b. in specified b. Materials in “commingled”1C010.a., with specified other fibres 1C010.b. or 1C010.c.; a. in 1C008 Resin or pitch, specified or 1C009.b.; Tg)’ (DMA temperature transition glass Analysis Mechanical b. ‘Dynamic b. Organic or carbon “fibrous or filamentary materials”, having of the all b. materials”, filamentary or Organic or carbon “fibrous a. Inorganic “fibrous or filamentary materials” specified in 1C010.c.; in specified materials” filamentary or “fibrous a. Inorganic 1. Composed of any of the following: 2. Assessing the “specific tensile strength”, “specific modulus” or specific Composed of materials specified in 1C010.d.1.a.2. or 1C010.d.1.b. and 2. Having any of the following: the of any 2. Having materials” (prepregs), metal or carbon-coated “fibrous or filamentary materials” materials” or filamentary carbon-coated “fibrous or metal (prepregs), materials” following: having of the all preforms”, or “carbon fibre (preforms) following: the of any 1. Having e. “fibrous or filamentary or pitch-impregnated resin-impregnated Fully or partially d. having any materials”, of the following: “Fibrous or filamentary

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m (determined by measurement techniques by such as measurement m (determined μ (CAS 7440-41-7), magnesium (CAS 7439-95-4) or alloys of these, at least if volume or weight are made up by of particle particles % of the total 90 particles of less than 60 M4C2d Metal powders of any of the (CAS following: zirconium 7440-67-7), beryllium )’ for )’ g

and ;

2 m whether spherical, atomised, sphe spherical, m whether μ

materials” (prepregs) for the repair of “civil aircraft” structures or aircraft” structures materials” (prepregs) for the repair of “civil laminates, having the following; all m 1 exceeding not area 1. An 3. A width exceeding 15 mm. 15 exceeding width 3. A chopped,cally milled or cut carbon “fibrous or filamentary in length when using a resin or pitch mm or less materials” 25,0 by 1C008 other than those specified or 1C009.b. 2. A length not exceeding 2,5 m; 2,5 exceeding not length 2. A

or “carbon preforms”,not impregnated fibre or pitch, are with resin specified by “fibrous or filamentary materials” in 1C010.a., 1C010.b. or 1C010.c. a. Epoxy resin “matrix” impregnated carbon “fibrous or filamentary or “fibrous carbon impregnated “matrix” resin a. Epoxy b. or partially resin-impregnated Fully or pitch-impregnated mechani- equal to or exceeding 505 K (232 °C) and having a resin or pitch, not equal to or exceeding 505 K (232 specified in 1C008 or 1C009.b., and not being a phenolic resin; c. ‘Dynamic Mechanical Analysis glass transition temperature (DMA Tg)’ (DMA temperature transition glass Analysis Mechanical c. ‘Dynamic Note 1: Note or carbon-coated materials” (preforms) “fibrous or filamentary Metal Note 2: 1C010.e. does not control: Technical Note: T temperature (DMA glass transition Analysis The ‘Dynamic Mechanical % or consisting roidal, flaked or ground, of 99 material manufactured from more of zirconium, magnesium and alloys thereof; materials specified by 1C010.e. is determined using the method described in by 1C010.e. determined using the materials specified is the ASTM D 7028-07, specimen. In national standard, or equivalent dry test on a case specimen shall be a of thermoset materials, degree of cure a dry test % as defined by ASTM E 2160-04 national or equivalent minimum of 90 standard. a. Metals in particle sizes of less than 60 than less of sizes particle in a. Metals N.B.: SEE ALSO 1C111. ALSO N.B.: SEE 1C011 Metals and compounds, as follows: as compounds, and 1C011 Metals

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m μ

in which one or more modes powder are controlled, the entire mixture is controlled. in which one or more modes powder are controlled, the entire mixture is controlled. designed for reduced or tailored reflectivity or emissivity in the microwave, in or emissivity designed for reduced or tailored reflectivity spectra. infrared or ultraviolet content of 85 % or more by weight, if at least 90 % of the total particles by particles % of the total 90 % or more by at least weight, if content of 85 volume of less than 60 made up or weight are particle of particles (determined by techniques measurement such as using a sieve, laser diffraction or ground; or optical scanning), atomised, spheroidal, flaked whether spherical, using a sieve, laser diffraction or optical scanning), whether spherical, atomised, spherical, scanning), whether optical or diffraction laser sieve, using a % by weight or more of any spheroidal, of flaked or ground, the consisting of 97 metals; above mentioned Note: grain sizes) of different (e.g. mixtures distribution a multimodal particle In Technical Note: % The natural content of hafnium 2 (CAS 7440-58-6) in the zirconium (typically is counted %) with the zirconium. to 7 technology), signatures and signatures (i.e. stealth acoustic for applications usable 1.A. in or 19.A. in 2.A. the systems specified subsystems for or the specified Note: grain sizes) of different (e.g. mixtures distribution a multimodal particle In signatures and acoustic signatures (i.e. stealth technology), signatures and (i.e. stealth for applications acoustic signatures in 1.A. usable for the systems specified or 19.A. in or the subsystems specified 20.A. 2.A. or Notes: specially paints), (including coatings and materials structural includes 1. 17.C.1. M4C2e boron a with boron alloys 7440-42-8) or boron (CAS either powders of Metal M17C1 Materials for reduced observables such as radar reflectivity, ultraviolet/infrared reflectivity, radar as such observables reduced for M17C1 Materials M17A1 Devices for reduced observables such as radar reflectivity, ultraviolet/infrared ultraviolet/infrared reflectivity, radar as such observables reduced for M17A1 Devices

m or less, as follows: μ

reflectivity; reflectivity or emissivity in the microwave, infrared or ultraviolet spectrum. electromagnetic the regions of the metals or alloys are encapsulated in aluminium, magnesium, zirconium or beryllium. the metals or alloys are encapsulated the metals in aluminium, magnesium, zirconium or beryllium. a. Structural materials and coatings specially designed for reduced radar reduced for designed specially coatings and materials a. Structural tailored or reduced for designed specially paints, including b. Coatings, substances to form a mixture formulated for military purposes. military formulated for mixture a form substances to Note: The metals or alloys specified in 1C011.a. are controlled whether or not or whether controlled are 1C011.a. in specified alloys or metals Note: The Technical Note: The natural content of hafnium 2 in the zirconium % to 7 (typically is counted %) with the zirconium. 1. Boron with a purity of 85 % by 1. weight or more; Boron with a purity of 85 % by weight or more; 2. Boron boron alloys with a content of 85 Note: in 1C011.b. The metals or alloys specified are controlled whether or not b. Boron of 60 size or boron alloys, with a particle Note 1: 1C101 includes: c. Guanidine nitrate (CAS 506-93-4); (CAS nitrate c. Guanidine 556-88-7). (CAS (NQ) d. Nitroguanidine N.B.: See also Goods Military Controls for metal powders mixed with other infrared signatures and acoustic signatures, other than those specified in 1C001, in specified vehicles subsystems unmanned or aerial “missile” ‘missiles’, usable in 9A112.a. 9A012 or 1C101 Materials and devices for reduced observables such as radar reflectivity, ultraviolet/ ultraviolet/ reflectivity, radar as such observables reduced for devices and 1C101 Materials

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m) or less, usable for rocket m) or less, usable for μ m (100

-6

greater; or mm or greater; and a length of 50 mm or greater 25 thermal control of satellites. vehicle nose tips usable in systems specified in 1.A. vehicle nose specified or 19.A.1. tips usable in systems nozzles and re-entry vehicle nose tips, which the any of nose tips, can be machined to vehicle nozzles and re-entry following products: mm or a. and a length of 50 mm or greater of 120 Cylinders having a diameter thickness of wall and a mm or greater b. of 65 Tubes having diameter an inner mm or greater mm × 50 c. mm × 120 Blocks having of 120 a size from 100 MHz to 100 GHz) for use in missile radomes usable in systems use in missile GHz) for MHz to 100 from 100 specified in 1.A. or 19.A.1. and having a grain size of 100 × 10 × 100 of size grain and having a 2. 17.C.1. does not control coatings (including paints) when specially used for used specially when paints) (including coatings control not does 2. 17.C.1. Designed for rocket systems; and b. Usable in the systems specified in 1.A. or in specified systems the in and b. Usable systems; rocket Designed for 19.A.1. M6C4 Pyrolytic or fibrous reinforced graphites usable for rocket nozzles and reentry and nozzles rocket for usable graphites reinforced fibrous or M6C4 Pyrolytic M6C5 Ceramic composite materials (dielectric constant less than 6 at any frequency any at 6 than less constant (dielectric materials composite M6C5 Ceramic M6C3 °C at 15 measured g/cc 1,72 bulk least with a graphites density of at Fine grain M6C2 Resaturated pyrolised (i.e. carbon-carbon) materials having all of the following: a. following: the of all having materials carbon-carbon) (i.e. pyrolised M6C2 Resaturated

or or greater, measured at or greater,

3 m or less, usable for rocket usable for m or less, μ

control of satellites. greater; mm or greater; and a length of 50 mm or greater 25 N.B.: See also 0C004 also N.B.: See vehicle nose tips usable in “missiles”, space launch vehicles specified in 9A004 specified launch vehicles space usable in “missiles”, nose vehicle tips or sounding in 9A104;rockets specified 3. Blocks having a size of 120 mm × 120 mm × 50 mm or greater; mm × 50 mm × 120 3. Blocks having of 120 a size space use in radomes usable “missiles”, GHz) for MHz to 100 from 100 launch vehicles specified in 9A004 or sounding rockets specified in 9A104; N.B.: See also 0C004 also N.B.: See 288 K (15 °C), and having a grain size of 100 of size grain a having and °C), (15 288 K the of any to be machined which can nose tips, vehicle and re-entry nozzles following products: 1. mm or and a length 50 of mm or greater 120 Cylinders of having a diameter of thickness wall a and greater or mm 65 of diameter inner an having 2. Tubes a. Fine grain graphites with a bulk density of 1,72 g/cm 1,72 of density bulk a with graphites grain a. Fine reentry and nozzles rocket for usable graphites, reinforced fibrous or b. Pyrolytic c. Ceramic composite materials (dielectric constant less than 6 at any frequency any at 6 than less constant (dielectric materials composite c. Ceramic Note 2: thermal 1C101 the used for does not include coatings when specially Note Technical Note: and In 1C101 systems means rocket unmanned complete ‘missile’ aerial vehicle km. systems capable of a range exceeding 300 specified in 9A004 or sounding rockets in specified 9A104. 1C107 Graphite and ceramic materials, other than those specified in 1C007, as follows: as 1C007, in specified those than other materials, ceramic and 1C107 Graphite 1C102 Resaturated pyrolized carbon-carbon materials designed for space launch vehicles launch space for designed materials carbon-carbon pyrolized 1C102 Resaturated

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m) and an aluminium content of 97 % by weight or m) and an aluminium content of 97

μ m (determined by measurement techniques by such as measurement m (determined μ m (ISO R-565) corresponds to 250 or 230 mesh (Tyler) μ m (200

-6

in which one or more modes powder are controlled, the entire mixture is controlled. m, according to ISO 2591-1:1988 to ISO m, according national equivalents; or less than 200 × 10 less than 200 vehicles, nozzle flaps, usable in systems specified in 1.A. specified or 19.A.1. usable in systems vehicles, nozzle flaps, (CAS 7440-41-7), magnesium (CAS 7439-95-4) or alloys of these, at least if volume or weight are made up by of particle particles % of the total 90 particles of less than 60 spherical, whether scanning), optical or diffraction laser sieve, using a by % weight or more or ground, atomised, spheroidal, flaked consisting of 97 of any above of the mentioned metals; Note: grain sizes) of different (e.g. mixtures distribution a multimodal particle In usable in systems specified in 1.A. or 19.A.1.; usable in systems specified more, if at least 10 % of the total weight is made up of particles of less than 63 of less particles made up of weight is total % of the 10 at least more, if μ Technical Note: 63 of size A particle standard E-11). mesh (ASTM M4C2c Spherical or spheroidal aluminium powder (CAS 7429-90-5) in particle size of size particle in 7429-90-5) (CAS powder aluminium spheroidal or M4C2c Spherical M6C6a Bulk machinable silicon-carbide reinforced unfired ceramic usable for nose tips nose for usable ceramic unfired reinforced silicon-carbide machinable M6C6a Bulk M6C6b Reinforced silicon-carbide ceramic composites usable for nose tips, re-entry tips, nose for usable composites ceramic silicon-carbide M6C6b Reinforced M4C2d Metal powders of any of the (CAS following: zirconium 7440-67-7), beryllium m and an μ m, according to ISO 2591- ISO m, according to μ

m (determined by measurement techniques by such as measurement m (determined μ m (ISO R-565) corresponds to 250 mesh (Tyler) or 230 corresponds R-565) to 250 m (ISO mesh (Tyler)

μ or mesh (ASTM standard E-11). mesh (ASTM follows: if at least 90 % of the total particles by particle volume or weight are made up volume or weight are by particle particles total % of the 90 least at if of less than 60 of particles atomized, spherical, whether scanning), optical or diffraction laser sieve, using a % by weight or more of any of the spheroidal, or ground, flaked consisting 97 following: 1. Zirconium; 2. Beryllium; vehicles and nozzle flaps usable space launch in “missiles”, vehicles specified in 9A004 or sounding in 9A104.rockets specified Military Goods Controls, size in particle of less than 200 total % of the 10 by at least % weight or more, if aluminium content of 97 weight of less than 63 is made up of particles equivalents; national 1:1988 or 3. Magnesium; Technical Note: 63 of size A particle usable in “missiles”, space launch vehicles specified in 9A004 specified space launch or sounding vehicles usable in “missiles”, in 9A104; rockets specified 1. Spherical or spheroidal aluminium powder other than that specified in the 2. Metal powders, other than that specified in the Military Goods Controls, as Military the in specified that than powders, other 2. Metal a. Metal powders of zirconium, beryllium or magnesium, or alloys of these metals, e. Reinforced silicon-carbide ceramic composites, usable for nose tips, reentry nose tips, for composites, usable ceramic silicon-carbide e. Reinforced d. nose usable for tips unfired ceramic, reinforced Bulk machinable silicon-carbide 1C011, as follows: 1C011, as substances: a. Propulsive 1C111 Propellants and constituent chemicals for propellants, other than those specified in specified those than other propellants, for chemicals constituent and 1C111 Propellants

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m μ

) that can ) that be used in

2 /NO 4

in which one or more modes powder are controlled, the entire mixture is controlled. missile systems. There a are range of compositions that can be denoted as MONi or MONij where i and the percentage of integers representing j are % Oxide, Nitric Nitric Oxide MON25 in the mixture (e.g. MON3 contains 3 25 % Nitric Oxide. An upper limit is MON40, 40 % by weight). Technical Note: in Oxide (NO) Nitric solutions of are (MON) Nitrogen Mixed Oxides of Dioxide (N Dinitrogen Tetroxide/Nitrogen Technical Note: % The natural content of hafnium (CAS 7440-58-6) 2 in the zirconium (typically counted is with the zirconium. %) to 7 Note: grain sizes) of different (e.g. mixtures distribution a multimodal particle In content of 85 % or more by weight, if at least 90 % of the total particles by particles % of the total 90 % or more by at least weight, if content of 85 volume of less than 60 made up or weight are particle of particles (determined by techniques measurement such as using a sieve, laser diffraction or ground atomised, spheroidal, flaked scanning), whether spherical, or optical 1. (CAS 10544-73-7) Dinitrogen trioxide 2. (CAS 10544-72-6); Nitrogen dioxide (CAS 10102-44-0) tetroxide dinitrogen / 3. Dinitrogen pentoxide (CAS 10102-03-1); (MON); Nitrogen of Oxides 4. Mixed M4C2e boron a with boron alloys 7440-42-8) or boron (CAS either powders of Metal M4C4a rocket engines as follows: Oxidiser substances usable in liquid propellant

) that can be used in

/NO

m (determined by measurement m (determined O μ 2

multimodal particle distribution (e.g. mixtures of different grain sizes) different of mixtures (e.g. distribution multimodal particle if one or more modes are controlled. Technical Note: (NO) in Oxides of Nitrogen Oxide (MON) are solutions Mixed of Nitric (N Dinitrogen Tetroxide/Nitrogen Dioxide missile systems. There are a range of compositions that can be denoted as MONi or MONij, where i and j are integers representing the percentage % Nitric Oxide, of Nitric Oxide in the mixture (e.g., MON3 contains 3 MON25 25 % Nitric Oxide. An upper limit is MON40, 40 % by weight). Technical Note: is counted to 7 %) 2 % The natural content of hafnium zirconium (typically in the with the zirconium. more by weight, if at least 90 % of the total particles by particle volume by or particle particles % of the total 90 least more by at weight, if of less than 60 weight are made up of particles a. Dinitrogen trioxide (CAS 10544-73-7); (CAS trioxide a. Dinitrogen 10544-72-6); (CAS tetroxide 10102-44-0)/dinitrogen (CAS dioxide b. Nitrogen 10102-03-1); (CAS pentoxide c. Dinitrogen (MON); Nitrogen of Oxides d. Mixed Note: 1C111a.2.a. a with and 1C111a.2.b.powder mixtures controls Note: techniques such as using a sieve, laser diffraction or optical scanning), whether optical or diffraction laser using sieve, techniques such a as spherical, atomised, spheroidal, flaked or ground; b. % or boron Metal powders or boron either of alloys with a boron content of 85 3. rocket engines as follows: Oxidiser substances usable in liquid propellant

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54- 2) in a gaseous state as it is not usable for missile applications. not usable 54- 2) in a gaseous is as for missile it state zinium azide (CAS 299177-50-7); nitrogen; Note: Item 4.C.4.a.6. does not control Nitrogen Trifluoride (NF3) (CAS 7783- (CAS (NF3) Trifluoride Nitrogen control not does 4.C.4.a.6. Note: Item 1. Monomethylhydrazine (MMH) (CAS 60-34-4); (CAS (MMH) 1. Monomethylhydrazine 57-14-7); (CAS (UDMH) dimethylhydrazine 2. Unsymmetrical 13464-97-6); (CAS mononitrate 3. Hydrazine 1741-01-1); (CAS 4. Trimethylhydrazine 6415-12-9); (CAS 5. Tetramethylhydrazine 5164-11-4); (CAS diallylhydrazine 6. N,N 7422-78-8); (CAS 7. Allylhydrazine 6068-98-0); (CAS dihydrazine 8. Ethylene dinitrate; 9. Monomethylhydrazine 10. Unsymmetrical dimethylhydrazine nitrate; dimethylhydrazine 10. Unsymmetrical 14546-44-2); (CAS azide 11. Hydrazinium 12. 1,1-Dimethylhydrazinium azide (CAS 227955-52-4) / 1,2-Dimethylhydra 13464-98-7); (CAS dinitrate 13. Hydrazinium 3457-37-2); (CAS dihydrazine acid oxalic 14. Diimido (HEHN); nitrate 15. 2-hydroxyethylhydrazine 27978-54-7); (CAS perchlorate 16. Hydrazinium 5. Inhibited Red Fuming Nitric Acid (IRFNA) (CAS 8007-58-7); (CAS (IRFNA) Acid Nitric Fuming Red 5. Inhibited 6. Compounds composed of fluorine and one or more of other halogens, oxygen or M4C2b Hydrazine derivatives as follows: as derivatives M4C2b Hydrazine

ARY GOODS CONTROLS AND ARY 1C238 FOR Compounds ARY GOODS CONTROLS Red Fuming Nitric FOR Inhibited ARY Acid (IRFNA); composed and fluorine one of or more of other halogens, oxygen or nitrogen; N.B.: SEE ALSO MILITARY GOODS CONTROLS. GOODS MILITARY ALSO N.B.: SEE 1741-01-1); (CAS a. Trimethylhydrazine 6415-12-9); (CAS 5164-11-4); b. Tetramethylhydrazine (CAS diallylhydrazine c. N,N 7422-78-8); (CAS d. Allylhydrazine dihydrazine; e. Ethylene dinitrate; f. Monomethylhydrazine nitrate; dimethylhydrazine 14546-44-2); g. Unsymmetrical (CAS azide h. Hydrazinium 13464-98-7); azide; (CAS i. Dimethylhydrazinium dinitrate j. Hydrazinium (HEHN); k. perchlorate; nitrate Diimido oxalic acid dihydrazine (CAS 3457-37-2); Hydrazinium for l. 2-hydroxyethylhydrazine Controls Goods 13812-39-0); Military m. See (CAS 29674-96-2); diperchlorate (CAS n. Hydrazinium (MHN) nitrate o. Methylhydrazine e. SEE MILIT e. SEE MILIT f. SEE 4. Hydrazine derivatives as follows: as derivatives 4. Hydrazine

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3 J/m

9 J/kg or greater; J/kg or

produced from vegetables, including fuels for engines certified for use for certified engines for fuels including vegetables, produced from in formulated for systems specified aviation, unless specifically in civil 1.A. or 19.A. (CAS 363453-17-2); solutions, JP-10) having a volume-based energy density of 37,5 × 10 × 37,5 of density energy volume-based having a solutions, JP-10) having a mass- based energy density of 40 × 10 × 40 of density energy based mass- having a Note: Item 4.C.2.f.2. does not control fossil refined fuels and biofuels or greater, measured at 20 °C and one atmosphere (101,325 kPa) pressure. measured at 20 or greater, 2. Other high energy density fuels and fuel additives (e.g., cubane, ionic 17. Hydrazinium diperchlorate (CAS 13812-39-0); (CAS diperchlorate 17. Hydrazinium 29674-96-2); (CAS (MHN) nitrate 18. Methylhydrazine 19. 1,1-Diethylhydrazine nitrate (DEHN) / 1,2-Diethylhydrazine nitrate (DEHN) (DHTN); nitrate tetrazine 20. 3,6-dihydrazino slurry, follows: boron as such fuels, liquid and solid both incorporate that fuels 1. Mixed (CAS 86147-04-8). Technical note: 1,4-dihydrazine nitrate. as to referred also is nitrate 3,6-dihydrazino tetrazine M4C2f in 1.A. specified usable in or 19.A., the systems High energy density materials, as M4C2g Hydrazine replacement fuels as follows: 1. 2-Dimethylaminoethylazide (DMAZ) 2-Dimethylaminoethylazide 1. follows: as fuels replacement M4C2g Hydrazine

3 J/m

J/kg or greater; greater; J/kg or

from vegetables, including fuels for engines certified for use in civil for engines from vegetables, including certified fuels or unmanned aerial formulated for ‘missiles’ aviation, unless specially vehicles specified in 9A012 or 9A112.a.. having a mass-based energy density of 40 × 10 × 40 of density energy mass-based having a produced biofuels and fuels refined fossil control not does Note: 1C111.a.5.b. solutions, JP-10) having a volume-based energy density of 37,5 × 10 × 37,5 density of having volume-based energy a solutions, JP-10) or greater, measured at 20 °C (101,325 and one atmosphere pressure; kPa) 20 at measured or greater, a. Mixed fuel that incorporate both solid and liquid fuels, such as boron slurry, Controls, or unmanned usable in 9A012 in ‘missiles’ vehicles specified aerial or boron as such fuels, 9A112.a.; liquid and solid both incorporate that fuel a. Mixed q. 3,6-dihydrazino tetrazine nitrate (1,4-dihydrazine nitrate) (DHTN); nitrate) (DEHN); (1,4-dihydrazine nitrate nitrate p. Diethylhydrazine tetrazine q. 3,6-dihydrazino b. Other high energy density fuels and fuel additives (e.g., cubane, ionic Technical Note: and In 1C111.a.5.systems unmannedmeans complete rocket aerial ‘missile’ km. vehicle systems capable of a range exceeding 300 86147-04-8); (CAS (DMAZ) a. 2-Dimethylaminoethylazide 5. High energy density materials, other than that specified in the Military Goods Military the in specified that than other materials, density energy 5. High 6. Hydrazine replacement fuels as follows: as fuels replacement 6. Hydrazine

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butadiene) (CTPB); butadiene) (HTPB); CAS 68891-50-9); Technical Note: Polytetrahydrofuran polyethylene glycol is a block (TPEG) co-polymer of poly 25322- (CAS (PEG) polyethylene glycol 110-63-4) and 1,4-Butanediol (CAS 68-3). a. poly — terminated carboxyl polybutadiene (including Carboxy — terminated b. poly polybutadiene (including hydroxyl Hydroxy — terminated — terminated (GAP); polymer azide c. Glycidyl (PBAA); Acid Acrylic — d. Polybutadiene e. (PBAN) (CAS 25265-19-4 / Acid — Polybutadiene Acrylonitrile — Acrylic (TPEG). glycol polyethylene f. Polytetrahydrofuran 27814-48-8) (CAS poly-GLYN) or (PGN nitrate g. Polyglycidyl a. Catocene (CAS 37206-42-1); (CAS a. Catocene 1273-89-8); (CAS ferrocene b. Ethyl ferrocene; c. Propyl 31904-29-7); (CAS ferrocene d. n-Butyl 1274-00-6); (CAS ferrocene e. Pentyl M4C5 Polymeric substances, as follows: as substances, M4C5 Polymeric M4C6c1 Carboranes, decaboranes, pentaboranes and derivatives thereof derivatives and pentaboranes decaboranes, M4C6c1 Carboranes, M4C6c2 Ferrocene derivatives, as follows: as derivatives, M4C6c2 Ferrocene

Technical Note: of co-polymer block a is (TPEG) glycol Polytetrahydrofuran polyethylene (CAS (PEG) poly 1,4-Butanediol110-63-4) and glycol (CAS polyethylene 25322-68-3). butadiene) (CTPB); Goods in the Military than specified butadiene) (HTPB), other that Controls; Carboranes, decaboranes, pentaboranes and derivatives thereof; derivatives and pentaboranes Carboranes, decaboranes, a. See Military Goods Controls for catocene; for Controls ferrocene; Goods Ethyl Military for a. See ferrocene; Controls Propyl Goods Military for b. See Controls ferrocene; Goods n-butyl Military for c. See ferrocene; Controls Pentyl Goods Military for d. See Controls Goods Military e. See SEE MILITARY GOODS CONTROLS FOR CONTROLS GOODS MILITARY SEE 6. Polyglycidyl nitrate (PGN or poly-GLYN) (CAS 27814-48-8). (CAS poly-GLYN) or (PGN nitrate 6. Polyglycidyl 1. Carboxy-terminated polybutadiene (including carboxyl-terminated poly poly hydroxyl-terminated polybutadiene (including 2. Hydroxy-terminated (PBAA); acid 3. Polybutadiene-acrylic (PBAN); acid-acrylonitrile 4. Polybutadiene-acrylic (TPEG); glycol polyethylene 5. Polytetrahydrofuran 1. 5. (CAS 693-21-0); (DEGDN) glycol dinitrate Diethylene M4C6d4 (DEGDN) (CAS 693-21-0) Diethylene glycol dinitrate 3. (CAS 119-75-5); 2-Nitrodiphenylamine M4C6e1 2-Nitrodiphenylamine (CAS 119-75-5); 6. Ferrocene derivatives as follows: as derivatives 6. Ferrocene 4. (TMETN) (CAS 3032-55-1); trinitrate Trimethylolethane M4C6d2 (TMETN) (CAS 3032-55-1); Trimethylolethane trinitrate 2. Triethylene glycol (TEGDN) (CAS 111-22-8); dinitrate M4C6d1 Triethylene glycol (TEGDN) (CAS dinitrate 111-22-8); c. Other propellant additives and agents: and additives propellant c. Other b. Polymeric substances: b. Polymeric

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- Ferrocenedicarboxylic acid ′ -diacetyl ferrocene (CAS -diacetyl ferrocene 1273-94-5); ′

six carbon aromatic functional group attached to the ferrocene molecule. 5,0 mm; or Note: Item 4.C.6.c.2.o does not control ferrocene derivatives that contain a contain that derivatives ferrocene control not does 4.C.6.c.2.o Note: Item (CAS 1293-87-4); than: or stage; annealed solution the in GPa 1. 0,9 2. and hardened stage; precipitation 1,5 GPa in the 1. Sheet, plate or tubing with a wall or plate thickness equal to or less than the following: greater or to equal °C, 20 at measured strength, tensile ultimate an a. Having forms: following the of b. Any f. Dicyclopentyl ferrocene (CAS 125861-17-8); (CAS ferrocene f. Dicyclopentyl ferrocene; g. Dicyclohexyl 1273-97-8); (CAS ferrocene h. Diethyl ferrocene; 1274-08-4); i. Dipropyl (CAS ferrocene 1,1 j. Dibutyl / 93894-59-8); (CAS 1271-55-2) ferrocene k. Dihexyl (CAS ferrocene l. Acetyl 1,1 / 1271-42-7) (CAS acid modifiers; carboxylic m. Ferrocene rate burning propellant rocket 125856-62-4); as (CAS usable n. Butacene derivatives ferrocene o. Other M6C8 in 1.A. or 19.A.1., usable in the systems specified Maraging steels, having of all M4C6d5 4,5 diazidomethyl-2-methyl-1,2,3-triazole (iso- DAMTR); (iso- diazidomethyl-2-methyl-1,2,3-triazole M4C6d5 4,5

-diacetyl ′

a six carbon ferrocene aromatic functional group a six the attached to molecule. specified in 1C111, Goods see the Military Controls. ferrocene; modifiers, other than those specified in the Military Goods Controls. Note: 1C111.c.6.o. does not control ferrocene derivatives that contain that derivatives ferrocene control not does Note: 1C111.c.6.o. specified in the Goods Military Controls. Note: For propellants and constituent chemicals for propellants not for For propellants and chemicals constituent Note: f. See Military Goods Controls for Dicyclopentyl ferrocene; Dicyclopentyl for Controls ferrocene; Goods Dicyclohexyl Military for f. See Controls ferrocene; ferrocene; Goods Diethyl Dipropyl Military for g. See Controls for ferrocene; Goods Controls Dibutyl Military h. See Goods for Military Controls i. See Goods ferrocene; Dihexyl Military for j. See Controls 1,1 / Goods ferrocene Military Acetyl k. See for Controls Goods Military l. See acids; carboxylic ferrocene butacene; for Controls for Goods Military m. See Controls Goods rate burning Military propellant rocket n. See as usable derivatives ferrocene o. Other 7. 4,5 diazidomethyl-2-methyl-1,2,3-triazole (iso- DAMTR), other than that than other DAMTR), (iso- diazidomethyl-2-methyl-1,2,3-triazole 7. 4,5 N.B.: SEE ALSO 1C216. ALSO N.B.: SEE 1C116 Maraging steels, useable in ‘missiles’, having all of the following: the of all having ‘missiles’, in useable steels, 1C116 Maraging

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 182 m) or less; μ

m (50

m) or less; μ -6

m (50

-6

containing 97 % by weight or more of tungsten; ii. Copper more of tungsten; ii. % by infiltrated weight or containing 97 % by weight or more of tungsten; Silver or iii. tungsten containing 80 % by weight or more of tungsten; and tungsten containing infiltrated 80 Tubes ii. mm or greater; and length of 50 a mm or greater of 120 diameter thickness of and a mm wall or greater having of 65 an inner diameter Blocks or iii. having mm or greater; and a length mm or greater of 50 25 mm or greater mm × 50 mm × 120 of 120 a size having an inner diameter equal to or greater than 270 mm. 270 than greater or to equal diameter inner having an 1. Any of the following material compositions: i. Tungsten and alloys 2. Able to be machined any the following products: i. Cylinders having of a 2. Tubular forms with a wall mm thickness and equal to or less than 50 weight or more and a particle size of 50 × 10 size of 50 weight or more and a particle substitutional elements or precipitates to produce or precipitates strengthening substitutional elements and agehar and alloy; the dening of and subsequently age hardened (precipi annealed stage) process (solution tation hardened stage). 97 % by weight or more and a particle size of 50 × 10 % by size of 50 weight or more and a particle 97 c. having of the following: all in the solid form Tungsten materials a. Tungsten and alloys in particulate form with a tungsten content of 97 % by % 97 of 1.A., 19.A.1. or 19.A.2, as follows:. content tungsten a with form particulate in alloys and a. Tungsten Technical Note: alloys: iron are Maraging steels a. Generally characterised by high nickel, very low carbon content and use transformation martensitic the facilitate to cycles treatment heat to b. Subjected b. Molybdenum and alloys in particulate form with a molybdenum content of content molybdenum a with form particulate in alloys b. Molybdenum and M6C7 components in of missile in the systems specified for the fabrication Materials

m) or less; μ m (50

m) or less; -6 μ m (50

-6

tungsten; or and or greater; or mm or greater; and a length of 50 mm or greater of 25 a. Tungsten and alloys containing 97 % by weight or more of tungsten; a. Tungsten and alloys containing 97 tungsten; of b. Copper more infiltrated ot tungsten % containing weight by 80 by weight or % more of 80 containing tungsten infiltrated c. Silver a. mm and a length of 50 mm or greater 120 of Cylinders having a diameter b. thickness and a wall mm or greater of 65 Tubes having an inner diameter greater. or mm by 50 mm by 120 mm c. 120 of size Blocks having a 1. Any of the following material compositions: material following the of 1. Any 2. Able to be machined to any following products: of the 97 % by weight or more and a particle size of 50 × 10 of 50 % by size weight or more and a particle 97 weight or more and a particle size of 50 × 10 of 50 size weight or more and a particle c. Tungsten materials in solid form having all of the following: the of all having form solid in materials c. Tungsten b. Molybdenum and alloys in form particulate with a molybdenum content of Technical Note: and In 1C117 systems means rocket unmanned complete ‘missile’ aerial vehicle km. systems capable of a range exceeding 300 a. Tungsten and alloys in particulate form with a tungsten content of 97 % by % 97 of content tungsten a with form particulate in alloys and a. Tungsten 1C117 Materials for the fabrication of ‘missiles’ components as follows: as components ‘missiles’ of fabrication the for 1C117 Materials

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) (CAS 7783-54-

2) in a gaseous state as it is not usable for missile applications. missile as it is not usable for 2) in a gaseous state percent nickel; structure ) of which at least 10 % is austenite by volume to (according structure ) of which at least 10 and equivalents); national ASTM E-1181-87 or or 3 mm or less. 1. Containing 17,0 – 23,0 weight percent chromium and 4,5 – 7,0 weight and chromium percent 1. Containing 17,0 23,0 weight – and percent; weight 0,10 than greater of content titanium a 2. Having micro two-phase a as to referred (also microstructure ferritic-austenitic 3. A 1. Ingots or bars having a size of 100 mm or more in each dimension; mm or more 1. Ingots or bars having a size of 100 of thickness 2. wall mm or less; mm or more and a thickness of 3 Sheets having a width of 600 a and more or mm 600 of diameter outer an having 3. Tubes equipment specified in 6.B.1. in equipment specified materials and handling of “production” the 4.B. for in equipment specified specified in 4.C. in 1.A. or 19.A.1. and having of the following: all characteristics: following the of all a. Having nitrogen; (NF Trifluoride Nitrogen control not does 4.C.4.a.6. Note: Item equipment specified in 6.B.1. in equipment specified b. Any of the following forms: following the of b. Any Missile Technology Control Regime (M.TCR): Equipment, software and technology annex M6C9 usable in the systems specified (Ti-DSS) steel duplex stainless Titanium-stabilized M6D1 “Software” specially designed or modified for the operation or maintenance of maintenance or operation the of for maintenance modified or or operation designed the specially for M6D1 “Software” modified or designed specially M4D1 “Software” M6D1 “Software” specially designed or modified for the operation or maintenance of maintenance or operation the for modified or designed specially M6D1 “Software”

and and of dual-use items ). M4C4a6 Compounds and composed one of other halogens, or more of fluorine oxygen or

3 structure) of which at least 10 percent is austenite by volume (according to equivalents); national ASTM E-1181-87 or percent nickel; or 3 mm or less. 1. Ingots or bars having a size of 100 mm or more in each dimension; mm or more 1. Ingots or bars having a size of 100 less; mm or 2. and mm or more a thickness of 3 Sheets having width of 600 a 3. A ferritic-austenitic microstructure (also referred to as a two-phase micro two-phase a as to referred (also microstructure ferritic-austenitic 3. A 1. Containing 17,0 and 4,5 chromium – 23,0 – 7,0 weight weight percent 1. percent; weight 0,10 than greater of content titanium a 2. Having 3. mm or more and a wall thickness of Tubes of 600 having an diameter outer

b. Having any of the following forms: following the of any b. Having “use” of equipment specified in 1B001 “use” of equipment specified to 1B003. 1B119. or 1B117, 1B118 in1B101, 1B102, 1B115, specified goods a. Having all of the following characteristics: characteristics: following the of all a. Having 1C238 Chlorine trifluoride (ClF trifluoride 1C238 Chlorine 1C118 following: the of having all (Ti-DSS) steel duplex stainless Titanium-stabilised 1D001 designed specially “development”,or modified for the “production” “Software” or 1D101 “Software” specially designed or modified for the operation or maintenance of maintenance or operation the for modified or designed specially 1D101 “Software” The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/ Council Regulation (EC) in identified corresponding equipment and components as systems, The 2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit and brokering transfer, exports, of control the for Community regime a 5 up setting 2009 of 2009 May 1D Software M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 184

reduction. reduction lation of temperature, pressures or atmosphere in autoclaves hydroclaves pressures when lation of temperature, used the production processed composites, for of composites usable or partially in 6.A. specified or 6.C for equipment or materials opment”, in 1.A., “production” specified or “use” of equipment or “software” 1.D. 1.B., or in specified “software” opment”,or “production”equipment, or “use” of materials 6.D. 6.C. or 6.A., 6.B., opment”, in 1.A., “production” specified or “use” of equipment or “software” 1.D. 1.B., or ultraviolet/infrared signatures and acoustic signatures (i.e. stealth technology), for applications usable for the systems specified in 1.A. or 19.A. or the subsystems specified in 2.A. Note: 17.D.1. includes specially “software” designed for analysis of signature opment”, “production” or “use” of equipment, materials or “software” specified in specified “software” opment”,or “production”equipment, or “use” of materials 17.D. 17.C. or 17.A., 17.B., Note: 17.E.1. includes databases specially designed for analysis of signature Missile Technology Control Regime (M.TCR): Equipment, software and technology annex M “Technology”, in accordance with the General Technology Note, for the “devel the for Note, Technology General the with accordance in M “Technology”, M “Technology”, in accordance with the General Technology Note, for the “devel the for Note, Technology General the with accordance in M “Technology”, M6E2 “Technical data” (including processing conditions) and procedures for the regu the for procedures and conditions) processing (including data” M6E2 “Technical M6E1 “Technology”, in accordance with the General Technology Note, for the “devel the for Note, Technology General the with accordance in M6E1 “Technology”, M17E1 “Technology”, in accordance with the General Technology Note, for the “devel the for Note, Technology General the with accordance in M17E1 “Technology”, M17D1 “Software” specially designed for reduced observables such as radar reflectivity, radar as such observables reduced for designed specially M17D1 “Software” of dual-use items

autoclaves or hydroclaves, when or used “production” the of “composites” for partially processed “composites”. specified in 1A102, 1B001, 1B101, 1B102, 1B115 to 1B119, 1C001, 1C101, 1B101, 1B102, 1B115 to 1A102, 1B001, in specified 1D103. or 1C118, 1D101 to 1C107, 1C111 in 1D001, specified 1D101 “software” or 1D103. “production” of equipment or materials specified in 1A001.b., specified “production” of equipment 1A001.c., or materials 1A002 to 1C. or 1A005, 1A006.b., 1A007, 1B reflectivity, ultraviolet/infrared signatures reflectivity, ultraviolet/infrared and acoustic signatures. 1E103 or atmosphere in pressure [M6E2]“Technology”the regulation of temperature, for 1E102 “Technology” according to the General Technology Note for the “development” of “development” the for Note Technology 1E101 General goods of the “use” Technology “Technology”General Note for the according to the to according 1E102 “Technology” 1E001 “Technology” according to the General Technology Note for the “development” or “development” the for Note Technology General the to according 1E001 “Technology” 1D103 designed of reduced observables such specially for analysis as radar “Software” The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/ Council Regulation (EC) in identified corresponding equipment and components as systems, The 2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit and brokering transfer, exports, of control the for Community regime a 5 up setting 2009 of 2009 May 1E Technology M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 185

Tolerance Class 2 (or ANSI/ABMA Std 20 Tolerance Class ABEC-9 or other and mm; the following characteristics: having or better all national equivalents), 50 and 12 between diameter bore ring inner a) An and mm; 100 and 25 between diameter outside ring outer b) An mm. 20 and 10 between width c) A

Missile Technology Control Regime (M.TCR): Equipment, software and technology annex M6E1 M3A7 Radial ball bearings having all tolerances specified in accordance with ISO 492 ISO with accordance in specified tolerances all having bearings ball M3A7 Radial

CATEGORY 2 — MATERRIALS PROCESSING — CATEGORY 2

of dual-use items

rates and process control schedules and parameters. schedules control and process rates in accordance with ISO 3290 as grade 5 or worse. than 414 MPa; manufacturer in accordance with ISO 492 Tolerance Class 4 (or national equiv Class 4 with ISO 492 in accordance (or Tolerance manufacturer and alents), or better, having both rings and rolling elements (ISO 5593), made from monel or beryllium; 3. High temperature (450 K (177 °C) and above) position sensors. 3. (450 K (177 High temperature Note: 2A001.a. does not control tapered roller bearings. roller tapered control not does Note: 2A001.a. greater strengths yield and greater or T 2,0 of densities flux with 1. Materials actuators; for designs bias homopolar 3D 2. All-electromagnetic formed on a mould, mandrel or other substrate from precursor gases which formed on from precursor a mould, or other substrate mandrel decompose in the 1 573 K of 130 at pressures Pa to 20 (1 300 kPa. °C) to 3 173 K 900 (2 °C) temperature range Note: 1E104 includes “technology” for the composition of precursor gases, flow- gases, precursor of composition the for “technology” includes Note: 1E104 a. Ball bearings and solid roller bearings, having all tolerances specified by the by specified tolerances all having bearings, roller solid and bearings a. Ball b. Not used; b. Not following: the of any using systems bearing magnetic c. Active N.B.: SEE ALSO 2A101. ALSO N.B.: SEE manufacturer the by specified tolerances with balls control not does Note: 2A001 1E104 derived materials “production” “Technology”to the of pyrolytically relating 2A001 Anti-friction bearings and bearing systems, as follows, and components therefor: components and follows, as systems, bearing and bearings 2A001 Anti-friction The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/ Council Regulation (EC) in identified corresponding equipment and components as systems, The 2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit and brokering transfer, exports, of control the for Community regime a 5 up setting 2009 of 2009 May

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 186

or greater; and or greater; numerical control units or a computer control, even when not equipped with and delivery; at such units a) Maximum working pressure equal to or greater than 69 MPa; 69 than greater or to equal °C pressure working 600 a) Maximum of environment thermal controlled a maintain and achieve to b) Designed greater. or mm 254 of diameter inside an with cavity chamber a c) Possessing Tolerance Class 2 (or ANSI/ABMA Std 20 Tolerance Class ABEC-9 or other and mm; the following characteristics: having or better all national equivalents), 50 and 12 between diameter bore ring inner a) An and mm; 100 and 25 between diameter outside ring outer b) An mm. 20 and 10 between width c) A a) According to the manufacturers technical specification can be equipped with equipped be can specification technical manufacturers the to a) According M6B3 Isostatic presses having all of the following characteristics: characteristics: following the of all having presses M6B3 Isostatic M3B3 Flow-forming machines, and specially designed components therefor, which: therefor, components designed specially and machines, M3B3 Flow-forming M3A7 Radial ball bearings having all tolerances specified in accordance with ISO 492 ISO with accordance in specified tolerances all having bearings ball M3A7 Radial or and

and

Military Goods Controls. degradation products. 2. A controlled thermal environment exceeding 1 773 K (1 500 °C); MPa; 500 207 exceeding (1 pressure working K maximum 1. A 773 1 exceeding environment thermal controlled 2. A with an inside diameter of 406 mm or more; of 406 with an inside diameter 3. A facility for hydrocarbon impregnation and removal of resultant gaseous resultant of removal and impregnation hydrocarbon for facility 3. A b. Having any of the following: the of any b. Having N.B.: 1B003, 9B009 and the see moulds and tooling designed dies, specially For components and accessories therefor: accessories components and cavity chamber a and cavity 2B204. and 2B104 closed ALSO N.B.: SEE the within environment thermal controlled a. A Technical Note: working which both the chamber in the of that is chamber dimension inside The temperature and working the pressure are achieved and does not include fixtures. That dimension will be the inside diameter of the smaller of either the pressure chamber, depending on furnace insulated the of diameter inside the chamber or which of the two chambers is located inside the other. specified in accordance with ISO 492 Tolerance Class 2 (or ANSI/ABMA Std 20 Class and ABEC-9 Tolerance having or other national equivalents), better the all mm; 50 following characteristics: and mm 12 between diameter bore ring inner a. An mm; 100 and mm 25 between diameter outside ring outer b. An c. A width between 10 mm and 20 mm. facturer's technical specification, can be equipped with “numerical control” units or can be equipped control” specification, with “numerical technical facturer's and a computer control following: having of the all 2B209. AND 2B109 ALSO N.B.: SEE 2B004 Hot “isostatic presses” having all of the following, and specially designed specially and following, the of all having presses” “isostatic 2B004 Hot 2B009 Spin-forming machines and flow-forming machines, which, according to the manu the to according which, machines, flow-forming and machines 2B009 Spin-forming 2A101 in 2A001, tolerances than those specified having all bearings, other ball Radial

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 187

duction” of propulsion components and equipment for motor (e.g. cases) systems specified in 1.A. duction” of propulsion components and equipment for motor (e.g. cases) systems specified in 1.A. or greater; and or greater; numerical control units or a computer control, even when not equipped with and delivery; at such units contouring control. contouring control. a) Maximum working pressure equal to or greater than 69 MPa; 69 than greater or to equal °C pressure working 600 a) Maximum of environment thermal controlled a maintain and achieve to b) Designed greater. or mm 254 of diameter inside an with cavity chamber a c) Possessing a) According to the manufacturers technical specification can be equipped with equipped be can specification technical manufacturers the to a) According b) Have more than two axes which can be co-ordinated simultaneously for Note: This item does not include machines that are not usable in the “pro does not include machines that are usable in the This item Note: “pro does not include machines that are usable in the This item Note: Technical Note: spin-forming and flow-forming are, for the Machines combining function of the machines. flow-forming as regarded item, this purpose of of carbon-carbon composites. b) Have more than two axes which can be co-ordinated simultaneously for M6B3 Isostatic presses having all of the following characteristics: characteristics: following the of all having presses M6B3 Isostatic M3B3 Flow-forming machines, and specially designed components therefor, which: therefor, components designed specially and machines, M3B3 Flow-forming M6B4 Chemical vapour deposition furnaces designed or modified for the densification the for modified or designed furnaces deposition vapour M6B4 Chemical

and

and and

“contouring control”. “contouring control”. with “numerical control” units or a computer control, even with when “numerical not units; such equipped with control”; 2. With more than two axes which can be coordinated simultaneously for or 2B109.a. (600 °C) or greater; 1. According to the manufacturer's technical specification, can be equipped c. Possessing a chamber cavity with an inside diameter of 254 mm or greater. mm or greater. c. of 254 Possessing with an inside diameter a chamber cavity Technical Note: For the purpose of 2B009, machines combining spin-forming the function of and machines. flow-forming are regarded as flow-forming a. Three or more axes which can be coordinated simultaneously for “contouring for simultaneously coordinated be can which axes more or a. Three kN. 60 than more force roller b. A b. Specially designed components for flow-forming machines specified in 2B009 in specified machines flow-forming for components designed b. Specially following: 2B204. ALSO N.B.: SEE a. Maximum working of 69 MPa or greater; pressure K 873 of environment thermal controlled a maintain and achieve to b. Designed follows: designed components as 2B209. ALSO N.B.: SEE following: the of all having machines a. Flow-forming 2B005.a., of carbon-carbon composites. designed the densification or modified for 2B109 Flow-forming machines, other than those specified in 2B009, and specially and 2B009, in specified those than other machines, 2B109 Flow-forming 2B104 “Isostatic presses”, other than those specified in 2B004, having all of the of all having 2B004, in specified those than other presses”, 2B104 “Isostatic 2B105 Chemical vapour deposition (CVD) furnaces, other than those specified in specified those than other furnaces, (CVD) deposition vapour 2B105 Chemical

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 188

incorporating a digital controller, capable of vibrating a system at an accel controller, incorporating a digital Hz and 2 kHz while g rms between 20 than eration equal to 10 or greater imparting forces equal to or than greater 50 kN, measured table’; ‘bare than control bandwidth’5 kHz greater and designed use with a ‘real-time for in 15.B.1.a.; systems specified with vibration test Technical Note: ‘Real-time control bandwidth’ is defined as the maximum rate at which a controller can of execute complete cycles sampling, processing data and transmitting control signals. than 50 kN, equal to or greater measured ‘bare a force capable of imparting in 15.B.1.a.; systems specified test and usable in vibration table’, shaker shaker units system capable of providing into a complete an effective and table’, ‘bare measured 50 kN, than greater or to equal combined force in 15.B.1.a. systems specified usable in vibration test 19.A.2. or the subsystems specified in 2.A. or 20.A., and components therefor, components and 20.A., or 2.A. in specified subsystems the 19.A.2. or as follows: systems employing or closed loop feedback techniques and a) Vibration test “software”, test vibration designed specially with combined controllers, b) Digital Technical Note: Machines combining spin-forming the function of and the flow-forming are, for machines. flow-forming as regarded item, this purpose of c) Vibration thrusters (shaker units), with or without associated amplifiers, multiple combine to designed units electronic and structures support piece d) Test M15B1 Vibration test equipment, usable for the systems specified in 1.A., 19.A.1. or 19.A.1. 1.A., in specified systems the for usable equipment, test M15B1 Vibration

propulsion components and equipment (e.g. motor cases) for systems for cases) motor (e.g. propulsion components and equipment specified in 9A005, 9A007.a. or 9A105.a. porating a digital controller, capable of vibrating a system at an acceleration vibrating a system at an acceleration capable of controller, porating a digital equal to or greater than 10 g rms forces equal to or greater than 50 kN, measured between ‘bare table’; 20 Hz and 2 kHz while imparting than 5 kHz designed use with bandwidth’for greater control with a ‘real-time in 2B116.a.; systems specified vibration test Technical Note: In 2B116.b., control bandwidth’‘real-time means the maximum rate at which a of sampling, processing cycles data complete and controller can execute trans mitting control signals. than and 50 kN, table’, equal to or greater measured ‘bare of imparting a force in 2B116.a.; systems specified usable in vibration test equal combined force of providing system capable an effective shaker units in a and systems usable in vibration than 50 table’, ‘bare kN, measured to or greater specified in 2B116.a. a. Vibration test systems employing feedback or closed loop techniques and incor and techniques loop closed or feedback employing systems test a. Vibration software, test vibration designed specially combined with controllers, b. Digital Note: production not usable in the of are 2B109 machines that does not control Technical Note: Machines combining function of spin-forming and the flow-forming are for the machines. flow-forming as 2B109 regarded purpose of c. Vibration thrusters (shaker units), with or without associated amplifiers, capable amplifiers, associated without or with units), (shaker thrusters c. Vibration multiple combine to designed units electronic and structures support piece d. Test 2B116 Vibration test systems, equipment and components therefor, as follows: as therefor, components and equipment systems, test 2B116 Vibration

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rotor mass; 1. Not capable of balancing rotors/assemblies having a mass greater than 3 kg; 3 than greater mass a having rotors/assemblies balancing of capable rpm; 1. Not 500 12 than greater speeds at rotors/assemblies balancing of 2. Capable 3. and unbalance in two planes or more; Capable of correcting 4. kg of g mm per 0,2 unbalance of specific residual a Capable of balancing to modified for use with machines specified in 9.B.2.a.;use with machines specified modified for Technical Note: the those systems, are incorporating controller a digital systems Vibration test stored and by controlled automatically entirely, or which are, partly functions of signals. digitally coded electrical characteristics: following the all having machines 1. Balancing of the following characteristics: more; or axes 1. Two designed or modified for densification and composite designed densification pyrolysis of structural or modified for vehicle nose rocket nozzles and tips. re-entry M6B5 Equipment and process controls, other than those specified in 6.B.3. or 6.B.4., or 6.B.3. in specified those than other controls, process and M6B5 Equipment M9B2a Equipment as follows: as M9B2a Equipment all having motion) simulating of capable (equipment tables simulators/rate M9B2c Motion M9B2b Indicator heads (sometimes known as balancing instrumentation) designed or designed instrumentation) balancing as known (sometimes heads M9B2b Indicator

dental or other medical equipment. rotor mass; Technical Note: Indicator heads known are sometimes as balancing instrumentation. capable of transferring electrical power, signal information, or both; power, and signal information, electrical capable of transferring 2B119.a. Note: 2B119.a. does not control balancing machines designed or modified for 1. Not capable of balancing rotors/assemblies having a mass greater than 3 kg; 3 than greater mass a having rotors/assemblies balancing of capable 1. Not 500 rpm; than 12 2. speeds greater at balancing rotors/assemblies Capable of 3. and unbalance in two planes or more; Capable of correcting kg of g mm per 4. 0,2 unbalance of specific residual a balancing to Capable of a. Two axes or more; or axes a. Two b. Designed non-contact devices or modified to incorporate slip rings integrated Technical Note: or fittings. In 2B116, means table, or surface, with no fixture a flat ‘bare table’ b. Indicator heads designed or modified for use with machines specified in b. 2B104 or 2B105, designed or modified for densification and pyrolysis of structural nose tips. vehicle nozzles and reentry composite rocket 2B219 ALSO N.B.: SEE characteristics: following the all having machines a. Balancing 2B120 having of the following characteristics: tables all Motion or rate simulators 2B117 Equipment and process controls, other than those specified in 2B004, 2B005.a., 2B004, in specified those than other controls, process and 2B117 Equipment 2B119 Balancing machines and related equipment, as follows: as equipment, related and machines 2B119 Balancing

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to or less than 0,6 degrees/s; 2. A rate resolution equal to or less than 6 degrees/s and an accuracy equal accuracy an and degrees/s 6 than 1. and of 400 more, or 30 or less; less or degrees/s Capable degrees/s of rates or to equal resolution rate 2. A % averaged over 10 or more; degrees minus 0,05 capable of transferring electrical power, signal information, or both; and electrical capable of transferring following: the of all having axis single any a. For b. Having equal stability than to a rate or (less) plus worst-case better or second. arc 5 than (better) less or to equal “accuracy” positioning c. A having the following characteristics: following having the and more; or axes second; 1. Two arc 5 than (better) less or to equal “accuracy” positioning 2. A modified to incorporate sliprings or integrated non-contact devices capable of sliprings or integrated modified to incorporate power, transferring electrical signal information, or both 2. Designed or modified to incorporate sliprings or integrated non-contact devices non-contact integrated or sliprings incorporate to modified or 2. Designed characteristics: following the of any 3. Having M9B2e Centrifuges capable of imparting accelerations above 100 g and designed or designed and g 100 above accelerations imparting of capable M9B2e Centrifuges M9B2d Positioning tables (equipment capable of precise rotary positioning in any axes) any in positioning rotary precise of capable (equipment tables M9B2d Positioning

and to or less than 0,6 degrees/s; tools or for medical equipment. For controls on machine tool rotary equipment. For controls tools or for medical tables see 2B008. whether or not slip rings or integrated non-contact devices are fitted at fitted are non-contact devices or integrated rings slip whether or not time of export. tools or for medical equipment. For controls on machine tool rotary equipment. For controls on machine medical tool or for tools tables see 2B008 or integrated non-contact devices are fitted at time of export are fitted or integrated non-contact devices b. A rate resolution equal to or less than 6 degrees/s and an accuracy equal accuracy an and degrees/s a. 6 Capable of 400 of rates or degrees/s more, or 30 than degrees/s or less; and less or to equal resolution rate b. A % averaged over 10 or more; degrees 0,05 1. For any single axis having all of the following: the of all having axis single any 1. For minus or plus than (less) better or to equal stability rate worst-case a 2. Having second. arc 5 than (better) less or to equal “accuracy” positioning 3. A b. A positioning “accuracy” equal to or less (better) than 5 arc second. arc 5 than (better) less or to equal “accuracy” positioning b. A Note: 2B121 does not control rotary tables designed or modified for machine non-contact devices capable of slip rings or integrated modified to incorporate power, transferring electrical signal information, or both. Note 1: Note 2B120 designed does not control rotary tables or modified for machine Note 2: Motion simulators or rate tables specified in 2B120 remain controlled c. Having any of the following characteristics: characteristics: following the of any c. Having Note: Centrifuges specified in 2B122 remain controlled whether or not slip rings slip not or whether controlled remain 2B122 in specified Note: Centrifuges other than those specified in 2B120, other than those specified having the following characteristics: all more; or axes a. Two 2B122 g and designed or above 100 accelerations of imparting capable Centrifuges 2B121 Positioning tables (equipment capable of precise rotary positioning in any axes), any in positioning rotary precise of capable (equipment tables 2B121 Positioning

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and flow-forming machines specified in 3.B.1. or 3.B.3. 3.B.1. or in specified machines and flow-forming duction” or “use” of a product. The may information of take the “technical form assistance”. data” or “technical 15.B. usable for testing systems specified in 1.A., 19.A.1. or 19.A.2. or 19.A.2. 19.A.1. or 1.A., in specified systems testing for 15.B. usable 20.A. 2.A. or in subsystems specified 6.B.4. or 6.B.5. 6.B.4. or Missile Technology Control Regime (M.TCR): Equipment, software and technology annex Missile Technology Control Regime (M.TCR): Equipment, software and technology annex M Means information which specific is required for the “development”, “pro M3D SOFTWARE M3D1 designed specially or modified for the “use” of “production “Software” facilities” M6D2 “Software” specially designed or modified for the equipment specified in 6.B.3., in specified equipment the for modified or designed specially M6D2 “Software” M15D1 designed in specially “use” of equipment or modified for the specified “Software”

of dual-use items of dual-use items

coordinate measurement machines specified in 2B006.a. in coordinate measurement machines specified “numerical control” codes for machining codes for various “numerical control” parts.

duction”in 2A001 of equipment specified or 2B001 2B009. 2B003 to 2A001.c., 2B001 or in

a. “Software” specially designed the “development” or “pro specially or modified for “Software” a. in 2A, specified equipment 2B or “software” or 2D. 2B104, 2B105, 2B109, 2B116, 2B117 or 2B119 to 2B122. to 2B119 2B117 or 2B104, 2B105, 2B109, 2B116, 9D004. ALSO N.B.: SEE 2E001 includes “technology” for the integration of probe systems into Note: Note: 2D001 does not control part programming “software” that generates b. designed of equipment specially or modified for the “use” specified “Software” 2E001 “Technology” according to the General Technology Note for the “development” of “development” the for Note Technology General the to according 2E001 “Technology” 2D001 “Software”, other than that specified in 2D002, as follows: as 2D002, in specified that than other 2D001 “Software”, 2D101 designed equipment in “use” of or modified for the specially specified “Software” The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/ Council Regulation (EC) in identified corresponding equipment and components as systems, The The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/ Council Regulation (EC) in identified corresponding equipment and components as systems, The 2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit and brokering transfer, exports, of control the for Community regime a 5 up setting 2009 of 2009 May 2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit and brokering transfer, exports, of control the for Community regime a 5 up setting 2009 of 2009 May 2D Software 2E Technology M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 192

duction” or “use” of a product. The may information of take the “technical form assistance”. data” or “technical duction” or “use” of a product. The may information of take the “technical form assistance”. data” or “technical Missile Technology Control Regime (M.TCR): Equipment, software and technology annex M Means information which specific is required for the “development”, “pro M Means information which specific is required for the “development”, “pro CATEGORY 3 — ELECTRONICS — CATEGORY 3

of dual-use items grated circuits; “Monolithic integrated circuits”; integrated “Monolithic circuits”; integrated “Hybrid circuits”; integrated “Multichip inte silicon-on-sapphire including circuits”, integrated type “Film “Optical integrated circuits”; integrated “Optical circuits”. integrated dimensional “Three — — — — — — function has been determined, is to be evaluated against the function has been determined, is 3A001.a. parameters of Note 2: the following types: include circuits Integrated Note 1: The control status of wafers (finished or unfinished), in which the (finished status of wafers The control 1: Note equipment specified in 2A or 2B. 2A or in equipment specified equipment or “software” specified in 2B004, 2B009, 2B104, 2B109, 2B116, 2B004, in specified “software” or equipment 2D101. or 2B122 2B119 to a. General purpose integrated circuits, as follows: as circuits, integrated purpose a. General 2E002 “Technology”“production”Technology the according to the General of Note for 2E101 “Technology” according to the General Technology Note for the “use” of 3A001 follows: as designed components therefor, specially components and Electronic The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/ Council Regulation (EC) in identified corresponding equipment and components as systems, The 2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit and brokering transfer, exports, of control the for Community regime a 5 up setting 2009 of 2009 May Components and Equipment 3A Systems, M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 193

+125 °C; and or have of the following characteristics: all a. °C to above from below range –54 operation in the temperature Rated for or sealed; b. Hermetically any of the following characteristics: following the any of a) ruggedised equipment; or for specifications military meet Designed to types: following the any of and being b) use military for modified Designed or unmanned aerial vehicles against nuclear effects (e.g. Electromagnetic Pulse Electromagnetic (e.g. effects nuclear against vehicles unmanned aerial and (EMP), X-rays, combined usable the systems for blast and effects), thermal specified in 1.A. unmanned aerial vehicles against nuclear effects (e.g. Electromagnetic Pulse Electromagnetic (e.g. effects nuclear against vehicles unmanned aerial and (EMP), X-rays, combined usable the systems for blast and effects), thermal specified in 1.A. Technical Note: that device or chemical optical is defined as a mechanical, electrical, A ‘detector’ a stimulus such and as an environ records, or registers automatically identifies signal mental change or electromagnetic in pressure or temperature, an electrical or that sense by one radiation from a material. This includes devices radioactive time operation or failure. M14A1 Analogue-to-digital converters, usable in the systems specified in 1.A., having 1.A., in specified systems the in usable converters, M14A1 Analogue-to-digital M18A1 “Radiation Hardened” “microcircuits” usable in protecting rocket systems and systems rocket protecting in usable “microcircuits” Hardened” M18A1 “Radiation M18A2 ‘Detectors’ specially designed or modified to protect rocket systems and systems rocket protect to modified or designed specially M18A2 ‘Detectors’ M14A1b1 1. Analogue-to-digital converter “microcircuits”, which are “radiation hardened” “radiation are which “microcircuits”, converter Analogue-to-digital M14A1b1 1.

2 n/cm

or Gy (silicon)/s or higher; or Gy (silicon)/s

6 Gy (silicon) or higher; or Gy (silicon)

3 Note: 3A001.a.1.c. does not control Metal Insulator Semiconductors (MIS). Semiconductors Insulator Metal control not does Note: 3A001.a.1.c. or higher on materials; silicon, or its equivalent for other specifications for ruggedized equipment; the following: 10 × 5 of dose total a. A b. A dose rate upset of 5 × 10 × 5 of upset rate dose b. A c. × 10 neutrons flux) of of 5 (1 MeV equivalent) (integrated A fluence 3A001, as follows: 3A001, as military meet to designed “missiles”, in usable converters, a. Analogue-to-digital 1. Integrated circuits designed or rated as radiation hardened to withstand any of as radiation 1. rated designed or circuits Integrated 3A101 Electronic equipment, devices and components, other than those specified in specified those than other components, and devices equipment, 3A101 Electronic

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rocket systems or unmanned that are not aerial vehicles capable of a km. “range”or greater than 300 equal to purposes. +80 °C; and modules, having all of the following characteristics: following the of modules, having all a. °C to above from below range –45 operation in the temperature Rated for 14.A.1.b.1. in specified “microcircuits” b. Incorporating strahlung electrons of from accelerated 2 MeV or greater, and equipment 1.A., 19.A.1. in specified systems the for usable accelerators, containing those or 19.A.2. in 2.A. or the subsystems or 20.A. specified or 19.A.2. Note: Item 12.A.6. does not control thermal batteries specially designed for Technical Note: In Item 15.B. table’ means ‘bare a flat table, or surface, with no or fixture fittings. Technical Note: that contain Thermal are single use batteries a solid non-conducting batteries material pyrolytic incorporate a batteries These electrolyte. the as inorganic salt battery. the and activates electrolyte the melts when ignited, that, Note: 15.B.5. does not control equipment specially designed for medical equipment specially 15.B.5. control does not Note: M15B5 Accelerators capable of delivering electromagnetic radiation produced by brems by produced radiation electromagnetic delivering of capable M15B5 Accelerators M12A6 Thermal batteries designed or modified for the systems specified in 1.A., 19.A.1. 1.A., in specified systems the for modified or designed batteries M12A6 Thermal M14A1b2 2. Electrical input type analogue-to-digital converter printed circuit boards or boards circuit printed converter analogue-to-digital type input Electrical M14A1b2 2.

medical purposes. Note: 3A101.b. above does not specify equipment specially designed for bremsstrahlung from accelerated electrons of 2 and MeV systems electrons or greater, accelerated bremsstrahlung from containing those accelerators. conducting inorganic salt as the electrolyte. These batteries incorporate a incorporate batteries These electrolyte. the as conducting inorganic salt pyrolytic material that, when and ignited, melts the electrolyte activates the battery. km. systems capable of a range exceeding 300 Technical Notes: 1. that contain a solid non- use batteries are single In 3A102 batteries’ ‘thermal vehicle aerial unmanned and systems rocket complete means ‘missile’ 3A102 2. In b. Accelerators capable of delivering electromagnetic radiation produced by 3A102 ‘Thermal batteries’ designed or modified for ‘missiles’. for modified or designed batteries’ 3A102 ‘Thermal

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 195

duction” or “use” of a product. The may information of take the “technical form assistance”. data” or “technical opment”, “production” or “use” of specified in 15.B. equipment or “software” or 15.D. 3A101.b. duction” or “use” of a product. The may information of take the “technical form assistance”. data” or “technical Missile Technology Control Regime (M.TCR): Equipment, software and technology annex Missile Technology Control Regime (M.TCR): Equipment, software and technology annex M Means information which specific is required for the “development”, “pro M Means information which specific is required for the “development”, “pro M15E1 “Technology”, in accordance with the General Technology Note, for the “devel the for Note, Technology General the with accordance in M15E1 “Technology”, M15D1 designed in specially “use” of equipment or modified for the specified “Software”

and m; μ

of dual-use items of dual-use items duction” of integrated circuits specified in 3A001.a.3. specified duction” of integrated circuits to 3A001.a.12., following: the of having all 0,130 above or at “technology” a. Using b. Incorporating with three or structures fewer metal layers. multi-layer or components controlled by 3A003. or components by controlled

equipment or “software” specified in 3A001.a.1. specified equipment or “software” or 2., 3A101, 3A102 or 3D101. in 3D101. specified “software” 3A101.b. in 3A, specified 3B “production”or 3C; of equipment or materials Note 1: 3E001 does not control “technology” for the “production” of equipment Note 2: 3E001 2: does not control “technology”the “development” or “pro for Note 3E102 “Technology” according to the General Technology Note for the “development” of “development” the for Note Technology 3E101 “Technology” General according to the General Technology Note for the “use” of the to according 3E102 “Technology” 3E001 “Technology” according to the General Technology Note for the “development” or “development” the for Note Technology General the to according 3E001 “Technology” 3D101 designed equipment in “use” of or modified for the specially specified “Software” The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/ Council Regulation (EC) in identified corresponding equipment and components as systems, The The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/ Council Regulation (EC) in identified corresponding equipment and components as systems, The 2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit and brokering transfer, exports, of control the for Community regime a 5 up setting 2009 of 2009 May 2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit and brokering transfer, exports, of control the for Community regime a 5 up setting 2009 of 2009 May 3D Software 3E Technology M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 196

+55 °C; or or modified for use in the systems specified in 1.A., in systems specified use in the having or modified for any the following of above to characteristics: °C –45 below from temperatures at operation continuous for a) Rated b) hardened”. “radiation ruggedised or Designed as Missile Technology Control Regime (M.TCR): Equipment, software and technology annex M13A1 analysers, designed Analogue computers, digital computers or digital differential

CATEGORY 4 — COMPUTERS — CATEGORY 4

Error/bit/day;

–8 Gy (silicon)/s;

Gy (silicon);

or of dual-use items 3

automobile, railway train or “civil aircraft” applications. aircraft” “civil or train automobile, railway applications. aircraft” ‘Vector processors’; ‘Vector processors; Array processors; signal Digital — — — a. Total Dose 5 × 10 × 5 Dose a. Total above 358 K (85 °C); (85 K above 358 Note: 4A001.a.1. does not control computers specially designed for civil “civil for designed specially computers control not does Note: 4A001.a.2. c. Single Event Upset 1 × 10 × 1 Upset Event c. Single b. Dose Rate Upset 5 × 10 × 5 Upset Rate b. Dose 2. Radiation hardened to exceed any of the following specifications: following the of any exceed to hardened 2. Radiation 1. Rated for operation at an ambient temperature below 228 K (–45 °C) or below 228 K (–45 ambient temperature an at operation 1. Rated for a. Specially designed to have any of the following: the of any have to designed a. Specially b. Not used. b. Not “electronic assemblies” and “electronic assemblies” specially designed components therefor: 4A101. ALSO N.B.: SEE Note 1: following: 4A003 the includes follows and specially designed follows and specially components therefor: 4A001 and following the equipment, having any of and related computers Electronic 4A003 as equipment therefor, and related assemblies”, “electronic computers”, “Digital The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/ Council Regulation (EC) in identified corresponding equipment and components as systems, The 2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit and brokering transfer, exports, of control the for Community regime a 5 up setting 2009 of 2009 May Components and Equipment 4A Systems, M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 197

+80 °C; and modules, having all of the following characteristics: following the of modules, having all above to °C –45 below from range temperature the in operation for a) Rated 14.A.1.b.1. in specified “microcircuits” b) Incorporating M13A1b hardened”. “radiation ruggedised or Designed as M14A1b2 Electrical input type analogue-to-digital converter printed circuit boards or boards circuit printed converter analogue-to-digital type input M14A1b2 Electrical

and

equipment for telecommunications equipment, see Category equipment, see equipment for telecommunications 1 (Telecommunications). 5, Part enhancement”designed equipment for other specially the required for those to functions limited equipment with the status of control the determined by other equipment is the “principal element” exceeds it other equipment even if criterion. N.B. 2: For the control status of “digital computers” or related is determined by 4E. N.B. 1: The control status of “signal processing” or “image operation of the other equipment or systems; other the operation of of the other equipment element” or systems; Logic processors; Logic enhancement”; “image for designed Equipment processing”. “signal for designed Equipment — — — c. The “technology” for the “digital computers” and related equipment described in 4A003 of other determined by the control status is provided: systems equipment or The “digital computers”a. or related equipment for the are essential equipment computers”are not a “principal or related b. The “digital specified in 3A001.a.5.; e. Equipment performing analogue-to-digital conversions exceeding the limits than those specified in 4A001.a.1., ruggedized and designed or than those specified which are use modified for in space in 9A004 launch vehicles specified or sounding in 9A104. rockets specified d. Not used d. Not Note 2: The control status of the “digital computers” and related equipment 2: Note 4A101 Analogue analysers, other computers, computers” “digital or digital differential

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specified in 16.D.1. This control only applies when the equipment is supplied with “software” simulation or design integration of systems specified in 1.A. of systems specified simulation or design or the subsystems integration specified in 2.A. Note: duction” or “use” of a product. The may information of take the “technical form assistance”. data” or “technical Missile Technology Control Regime (M.TCR): Equipment, software and technology annex M Means information which specific is required for the “development”, “pro M16A1 Specially designed hybrid (combined analogue/digital) computers for modelling, for computers analogue/digital) (combined hybrid designed M16A1 Specially

of dual-use items

specified in 7D103 or 9D103. exceeding 1,0 Weighted TeraFLOPS (WT); exceeding 1,0 Weighted TeraFLOPS performance by aggregation of processors so that the “APP” of the aggre in 4E001.b.1. gation exceeds the limit

opment”, in 4A “production” specified or “use” of equipment or “software” or 4D. the “development”“production” or modified for of equipment as follows: computers” having (“APP”) “Digital an “Adjusted Peak Performance” 1. 2. “Electronic assemblies” specially designed or modified for enhancing Note: This control only applies when the equipment is supplied with “software” with supplied is equipment the when applies only control Note: This gration of in 9A004 space launch vehicles specified or sounding rockets specified in 9A104. b. “Technology”, other than that specified in 4E001.a., specially designed or c. “Technology” for the “development” of “intrusion software”. 4E001 “Technology” according to the General Technology Note, for the “devel a. 4A102 “Hybrid computers” specially designed for modelling, simulation or design inte design or simulation modelling, for designed specially computers” 4A102 “Hybrid The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/ Council Regulation (EC) in identified corresponding equipment and components as systems, The 2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit and brokering transfer, exports, of control the for Community regime a 5 up setting 2009 of 2009 May 4E Technology M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 199

or satellites. terrestrial or marine applications. GNSS services. safety) flight integrity, (e.g. data of Life’

12.A.4. or 12.A.5., usable for systems specified in 1.A., 19.A.1. or 19.A.2. 19.A.1. or 1.A., in specified systems for 12.A.5., usable 12.A.4. or modified for systems specified in 1.A., systems specified 19.A.1. modified for or 19.A.2. Notes: aircraft manned for modified or designed equipment control not does 1. 12.A.4. for modified or designed equipment based ground control not does 2. 12.A.4. ‘Safety or civil commercial, for designed equipment control not does 3. 12.A.4. Missile Technology Control Regime (M.TCR): Equipment, software and technology annex Missile Technology Control Regime (M.TCR): Equipment, software and technology annex M12D3 designed in specially “use” of equipment or modified for the specified “Software” M12A4 equipment, including ground equipment, designed or and telecontrol Telemetry Part 1 — Telecommunications

CATEGORY 5 — TELECOMMUNICATIONS “INFORMATION— SECURITY”AND CATEGORY 5

of dual-use items of dual-use items

applications; GNSS integrity, flight safety) services; a. Equipment designed or modified for manned aircraft or satellites; or aircraft manned for modified or designed a. Equipment b. marine or terrestrial for Ground modified based equipment designed or c. Equipment designed (e.g. data or ‘Safety of Life’ for commercial, civil

Technical Note: and means systems unmanned In 5A101 complete rocket ‘missile’ aerial vehicle km. systems capable of a range exceeding 300 modified for ‘missiles’. modified for 5A101. Note: 5A101 does not control: not does Note: 5A101 5A101 equipment, including ground designed or telecontrol and Telemetry 5D101 designed equipment in “use” of or modified for the specially specified “Software” The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/ Council Regulation (EC) in identified corresponding equipment and components as systems, The The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/ Council Regulation (EC) in identified corresponding equipment and components as systems, The 2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit and brokering transfer, exports, of control the for Community regime a 5 up setting 2009 of 2009 May 2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit and brokering transfer, exports, of control the for Community regime a 5 up setting 2009 of 2009 May 5D1 Software Components and Equipment 5A1 Systems, M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 200

opment”, “production” or “use” of equipment or “software” specified in 12.A. specified opment”,or of equipment “software” “production” or “use” or 12.D. unmanned aerial vehicles against nuclear effects (e.g. Electromagnetic Pulse Electromagnetic (e.g. effects nuclear against vehicles unmanned aerial and (EMP), X-rays, combined usable the systems for blast and effects), thermal specified in 1.A. Technical Note: that device or chemical optical is defined as a mechanical, electrical, A ‘detector’ a stimulus such and as an environ records, or registers automatically identifies signal mental change or electromagnetic in pressure or temperature, an electrical or that sense by one radiation from a material. This includes devices radioactive time operation or failure Missile Technology Control Regime (M.TCR): Equipment, software and technology annex Missile Technology Control Regime (M.TCR): Equipment, software and technology annex M12E1 “Technology”, in accordance with the General Technology Note, for the “devel the for Note, Technology General the with accordance in M12E1 “Technology”, M18A2 ‘Detectors’ specially designed or modified to protect rocket systems and systems rocket protect to modified or designed specially M18A2 ‘Detectors’

CATEGORY 6 — SENSORS AND LASERS AND SENSORS — CATEGORY 6

of dual-use items of dual-use items

exceeding 300 nm; and nm; exceeding 300 nm; wavelength exceeding 400 plane arrays”. 1. A peak response in the wavelength range exceeding 10 nm but not but nm 10 exceeding range wavelength the in response peak 1. A peak response to the at a % relative than 0,1 A response of less 2. a. “Space-qualified” solid-state detectors having all of the following: Note: For the purpose of 6A002.a.1., solid-state detectors include “focal the of all having detectors solid-state a. “Space-qualified”

1. “Space-qualified” solid-state detectors as follows: as detectors solid-state 1. “Space-qualified” “production”in 5A101. or “use” of equipment specified N.B.: SEE ALSO 6A102. ALSO N.B.: SEE follows: as detectors a. Optical 5E101 “Technology” according to the General Technology Note for the “development”, the for Note Technology General the to according 5E101 “Technology” 6A002 Optical sensors or equipment and components as follows: therefor, The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/ Council Regulation (EC) in identified corresponding equipment and components as systems, The The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/ Council Regulation (EC) in identified corresponding equipment and components as systems, The 2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit and brokering transfer, exports, of control the for Community regime a 5 up setting 2009 of 2009 May 2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit and brokering transfer, exports, of control the for Community regime a 5 up setting 2009 of 2009 May 6A Systems, Equipment and Components and Equipment 6A Systems, 5E1 Technology M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 201

lisers, automatic pilots and inertial navigation systems. degrees) axes. latitudes of +/– 80 degrees, referenced to local magnetic field; and systems. gyrostabi include 9.A.8. Item in systems navigation and control Note: Flight (direction finding equipment) or terrain characteristics, designed or modified for characteristics, finding equipment) or terrain (direction in 1.A. systems specified use in the and specially designed components therefor: and specially 180 (+/– roll having and degrees) 90 (+/– pitch in compensation tilt a) Internal at rms degrees 0,5 than (less) better accuracy azimuthal providing of b) Capable c) Designed or modified to be integrated with flight control and navigation M9A8 Three axis magnetic heading sensors having all of the following characteristics, following the of all having sensors heading magnetic axis M9A8 Three M11A2 Passive sensors for determining bearings to specific electromagnetic sources electromagnetic specific to bearings determining for sensors M11A2 Passive

designed subsystems designed to reduce in-motion noise, and having in-motion a designed subsystems reduce to than per square equal root Hz 50 to fT (rms) or lower (better) ‘sensitivity’ Hz; at a frequency of 1 (better) than 20 pT (rms) per square root Hz at a frequency of 1 Hz 1 of frequency a at Hz root square per than 20 pT (rms) (better) in-motion noise; designed to reduce and specially cations or biomagnetic measurements for medical diagnostics. exceeding 1 200 nm; and nm; 200 exceeding 1 having any of the following: the having any of operation, without specially stationary SQUID systems designed for a. b. SQUID systems having an in-motion-magnetometer ‘sensitivity’ lower 1. A peak response in the wavelength range nm exceeding but 900 not 2. constant” of 95 A ns response “time or less; nm; 000 nm but not exceeding 30 200 range exceeding 1 nm array and having a peak response in the wavelength range exceeding 300 nm. exceeding 900 but not 1. “Magnetometers” using “Magnetometers” “superconductive” (SQUID) “technology” and 1. b. “Space-qualified” solid-state detectors having all of the following: the of all having detectors solid-state b. “Space-qualified” a. “Magnetometers” and subsystems as follows: as subsystems and a. “Magnetometers” underwater electric field sensors, field “compensation systems”, and underwater electric specially follows: as designed components therefor, 7A103.d. ALSO N.B.: SEE Note: 6A006 does not control instruments specially designed for fishery appli c. having a peak response wavelength detectors in the solid-state “Space-qualified” 048 per elements having than 2 more plane arrays” “focal d. “Space-qualified” 6A006 “Magnetometers”, “magnetic gradiometers”, “intrinsic magnetic gradiometers”, gradiometers”, magnetic “intrinsic gradiometers”, “magnetic 6A006 “Magnetometers”,

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(mgal); and 1. than 0,7 milligal (better) equal to or less accuracy or operational A static airborne or marine use, usable for systems specified in 1.A., as follows, and specially designed components therefor: following: the all having meters a) Gravity M12A3 Gravity meters (gravimeters) or gravity gradiometers, designed or modified for modified or designed gradiometers, gravity or (gravimeters) meters M12A3 Gravity

Gal; μ or

nT (rms) per square root Hz at frequencies exceeding 10 Hz; exceeding 10 frequencies square root Hz at per nT (rms) nT (rms) per square root Hz at frequencies of 1 Hz or more but more Hz or of 1 frequencies Hz at root square per nT (rms)

–4 –3 not exceeding 10 Hz; not exceeding 10 (rms) per square root Hz; c. 1 × 10 × c. 1 Overhauser) “technology” having than 20 lower a (better) ‘sensitivity’ pT (rms) per Hz; square root Hz at a frequency of 1 Hz; than 10 per square root Hz a frequency of 1 at pT (rms) or lower (better) Hz; 1 of the following: than less of frequencies at Hz root square per (rms) nT a. 0,05 10 × b. 1 6A006.a.; than lower 0,3 field ‘sensitivity’ (better) nT/m rms per square root Hz; (better) lower “technology”,‘sensitivity’ having field magnetic gradient a than 0,015 root Hz; per square rms nT/m 5. Fibre optic “magnetometers” having a ‘sensitivity’ lower (better) than 1 nT 1 than (better) lower ‘sensitivity’ a having “magnetometers” optic 5. Fibre 2. “Magnetometers” 2. “Magnetometers” using optically pumped or nuclear precession (proton/ 3. using “Magnetometers” fluxgate “technology” equal to having a ‘sensitivity’ any than (better) lower ‘sensitivity’ a having “magnetometers” coil 4. Induction accuracy of less (better) than 10 accuracy of less (better) resulting in a performance equal to or better than the specified parameters of parameters than the specified equal to or better in a performance resulting 6A006.c.; or 6A006.a., 6A006.b. nanovolt per metre per square root Hz when measured at 1 Hz; nanovolt per square root Hz when per metre measured at 1 in using specified “Magnetic gradiometers” multiple “magnetometers” 1. having gradient gradiometers” a magnetic magnetic optic “intrinsic Fibre 2. fibre-optic than other “technology” using gradiometers”, magnetic 3. “Intrinsic N.B.: SEE ALSO 6A107. ALSO N.B.: SEE a. Gravity meters designed or modified for ground use and having a static d. “Compensation systems” for magnetic or underwater electric field sensors b. Underwater electric field sensors having a ‘sensitivity’ lower (better) than 8 follows: as gradiometers” c. “Magnetic 6A007 Gravity meters (gravimeters) and gravity gradiometers, as follows: as gradiometers, gravity and (gravimeters) meters 6A007 Gravity

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2. of two minutes or less; registration A time to steady-state b) Gravity gradiometers. b) Gravity Technical Note: transmission, Laser radar embody specialised scanning, systems and receiving ranging, for echo direction lasers of utilisation for signal processing techniques and body speed radial location, by targets of and discrimination finding reflection characteristics. in the systems specified in 1.A. in the systems specified M11A1 Radar and laser radar systems, including altimeters, designed or modified for use for modified or designed altimeters, including systems, radar laser and M11A1 Radar

and

standards and employing electronically steerable linear (1-dimensional) linear steerable electronically standards and employing antennae. positioned passive mechanically arrays or (Worden) type. Secondary surveillance radar (SSR); radar surveillance Secondary Radar; Automotive Civil Displays or control (ATC); monitors used for air traffic radar; (weather) Meteorological Precision approach radar (PAR) equipment conforming to ICAO — — — — — ‘time-to-steady-state registration’ of less than 2 minutes under any of less registration’ ‘time-to-steady-state influences; and motional compensations corrective attendant combination of Technical Note: referred (also registration’ purposes 6A007.b., For the of ‘time-to-steady-state to as the gravimeter's response is the time over which time) the disturbing effects of platform induced accelerations (high frequency noise) are reduced. 2. An in-service (operational) accuracy of less (better) than 0,7 mGal having a having mGal 0,7 than (better) less of accuracy (operational) in-service 2. An Note: 6A007.a. does not control ground gravity meters of the quartz element quartz the of meters gravity ground control not does Note: 6A007.a. mGal; 0,7 than (better) less of accuracy static 1. A c. Gravity gradiometers. c. Gravity specially designed components therefor: 6A108. ALSO N.B.: SEE b. Gravity meters designed for mobile platforms and having all of the following: control: not does Note: 6A008 6A008 Radar systems, equipment and assemblies, having any of the following, and following, the of any having assemblies, and equipment systems, 6A008 Radar

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(mgal); and 1. than 0,7 milligal (better) equal to or less accuracy or operational A static less; or minutes two of registration steady-state to time 2. A airborne or marine use, usable for systems specified in 1.A., as follows, and specially designed components therefor: following: the all having meters a) Gravity gradiometers. b) Gravity all of the following capabilities: mrad; 1,5 than better resolution 1. Angular m rms; and 2. km with or greater a range than resolution better 10 Range of 30 m/s. 3 than better resolution 3. Velocity Technical Note: that device or chemical optical is defined as a mechanical, electrical, A ‘detector’ a stimulus such and as an environ records, or registers automatically identifies signal mental change or electromagnetic in pressure or temperature, an electrical or that sense by one radiation from a material. This includes devices radioactive time operation or failure. unmanned aerial vehicles against nuclear effects (e.g. Electromagnetic Pulse Electromagnetic (e.g. effects nuclear against vehicles unmanned aerial and (EMP), X-rays, combined usable the systems for blast and effects), thermal specified in 1.A. M12A3 Gravity meters (gravimeters) or gravity gradiometers, designed or modified for modified or designed gradiometers, gravity or (gravimeters) meters M12A3 Gravity M18A2 ‘Detectors’ specially designed or modified to protect rocket systems and systems rocket protect to modified or designed specially M18A2 ‘Detectors’ M12A5b Range instrumentation radars including associated optical/infrared trackers with trackers optical/infrared associated including radars instrumentation M12A5b Range

rads (silicon).

5 (better) in azimuth; airborne or marine use, equal to or and accuracy airborne or marine having or operational a static than regis and 0,7 (mgal), having less (better) milligal a time-to-steady-state of two tration minutes or less; 6A007.c. in specified gradiometers gravity 6A107.a. and Technical Note: plus the highest sum of of the equals one half operating frequency’ The ‘centre operating the lowest specified frequencies. 2. Locating accuracy of 1 m or less (better) in range and 0,2 or less degree less (better) m or 2. of 1 Locating accuracy following: mW; 100 exceeding power output average 1. An a. Operating at frequencies from 40 GHz to 230 GHz and having any of the GHz and having any of 230 to GHz 40 from frequencies at Operating a. designed modified for protecting against nuclear effects (e.g. electromagnetic (e.g. effects nuclear against protecting for designed modified “mis and usable for effects) and thermal combined blast X-rays, pulse (EMP), total or exceed a which meet levels to withstand designed radiation siles”, or rated × 10 irradiation dose of 5 a. Gravity meters, other than those specified in 6A007.b, designed or modified for modified or designed 6A007.b, in gradiometers, as follows: specified those than other meters, a. Gravity b. Specially designed components for gravity meters specified in 6A007.b or c. Capable of operating simultaneously on more than two carrier frequencies; carrier two than more on simultaneously operating of c. Capable Technical Note: or chemical optical as a mechanical, electrical, defined is In 6A102, a ‘detector’ and that automatically identifies records, a device or registers stimulus such as an electromagnetic or an electrical temperature, or pressure environmental change in that sense by This includes devices material. signal or radiation from a radioactive failure. operation or one time b. A tunable bandwidth exceeding ± 6,25 % of the ‘centre operating frequency’; operating ‘centre the of % 6,25 ± exceeding bandwidth tunable b. A 6A102 Radiation hardened ‘detectors’, other than those specified in 6A002, specially 6A002, in specified those than other ‘detectors’, hardened 6A102 Radiation 6A107 and Gravity meters (gravimeters) components for gravity meters and gravity

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and unmanned aerial vehicle in conjunction with either surface or airborne or surface either with conjunction in vehicle unmanned aerial references or navigation satellite systems to provide real-time measurements position of inflight and velocity; following capabilities: of the with all mrad; 1,5 than better resolution 1. Angular m rms; than 10 with a range resolution better km or greater 2. Range of 30 m/s. 3 than better resolution 3. Velocity 19.A.2. as follows: 19.A.2. as a. Tracking systems which use a code translator installed on the rocket or b. Range instrumentation radars including associated optical/infrared trackers in the systems specified in 1.A. in the systems specified Technical Note: transmission, Laser radar embody specialised scanning, systems and receiving ranging, for echo direction lasers of utilisation for signal processing techniques and body speed radial location, by targets of and discrimination finding reflection characteristics. M12A5 Precision tracking systems, usable for systems specified in 1.A., 19.A.1. or 19.A.1. 1.A., in specified systems for usable systems, tracking M12A5 Precision M11A1 Radar and laser radar systems, including altimeters, designed or modified for use for modified or designed altimeters, including systems, radar laser and M11A1 Radar

equipment; a. Terrain contour mapping equipment; a. Terrain equipment; sensor b. Imaging and analogue) digital mapping Scene (both and correlation c. radar equipment. navigation d. Doppler surface or airborne references or navigation satellite systems to provide or navigation satellite references or airborne surface real-time measurements of in-flight position and velocity; following capabilities: of the with all milliradians; 1,5 than better resolution a. Angular b. Range of m/s. 30 km or greater 3 with than a range better resolution resolution better than c. Velocity 10 m rms; 1. Tracking systems which use a code in translator conjunction with either trackers including 2. Range optical/infrared radars associated instrumentation Technical Note: and In 6A108.b. systems means unmannedcomplete rocket ‘missile’ aerial km. vehicle systems capable of a range exceeding 300 vehicles specified in 9A004 or sounding rockets specified in 9A104; following: the includes Note: 6A108.a. b. Precision tracking systems, usable for ‘missiles’, as follows: as ‘missiles’, for usable systems, tracking b. Precision follows: a. systems designed use in radar or modified for space launch Radar and laser 6A108 Radar systems and tracking systems, other than those specified in entry 6A008, as

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11.A.1., 11.A.2. or 11.A.4. or 11.A.1., 11.A.2. systems specified in 1.A., systems specified 19.A.1. or 19.A.2. or the subsystems in 2.A specified duction” or “use” of a product. The may information of take the “technical form assistance”. data” or “technical systems specified in 1.A., systems specified 19.A.1. or 19.A.2. or the subsystems in 2.A specified 12.A.4. or 12.A.5., usable for systems specified in 1.A., 19.A.1. or 19.A.2. 19.A.1. or 1.A., in specified systems for 12.A.5., usable 12.A.4. or Missile Technology Control Regime (M.TCR): Equipment, software and technology annex Missile Technology Control Regime (M.TCR): Equipment, software and technology annex M Means information which specific is required for the “development”, “pro M17B1 Systems, specially designed for radar cross section measurement, usable for the for usable measurement, section cross radar for designed specially M17B1 Systems, M17B1 Systems, specially designed for radar cross section measurement, usable for the for usable measurement, section cross radar for designed specially M17B1 Systems, M11D1 designed in specially “use” of equipment or modified for the specified “Software” M12D3 designed in specially “use” of equipment or modified for the specified “Software”

of dual-use items of dual-use items

6A108. Technical Note: and means systems unmanned In 6B108 complete rocket ‘missile’ aerial vehicle km. systems capable of a range exceeding 300 6B008. 6A008 or section measurement usable for ‘missiles’ and their subsystems. and their usable for ‘missiles’ section measurement 100 ns or less, and specially designed components therefor. designed specially and less, or 100 ns 6B108. ALSO N.B.: SEE 6B108 Systems, other than those specified in 6B008, specially designed for radar cross radar for designed specially 6B008, in specified those than other 6B108 Systems, 6B008 Pulse radar cross-section measurement systems having transmit pulse widths of widths pulse transmit having systems measurement cross-section radar 6B008 Pulse 6D102 “Software” specially designed or modified for the “use” of goods specified in specified goods of “use” the for modified or designed specially 6D102 “Software” 6D002 “Software” specially designed for the “use” of equipment specified in 6A002.b., in specified equipment of “use” the for designed specially 6D002 “Software” The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/ Council Regulation (EC) in identified corresponding equipment and components as systems, The The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/ Council Regulation (EC) in identified corresponding equipment and components as systems, The 2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit and brokering transfer, exports, of control the for Community regime a 5 up setting 2009 of 2009 May 2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit and brokering transfer, exports, of control the for Community regime a 5 up setting 2009 of 2009 May 6B Test, Inspection and Production Equipment Production and Inspection 6B Test, 6D Software M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 207

duction” or “use” of a product. The may information of take the “technical form assistance”. data” or “technical duction” or “use” of a product. The may information of take the “technical form assistance”. data” or “technical duction” or “use” of a product. The may information of take the “technical form assistance”. data” or “technical vehicle position designed throughout path, specially or modified for its flight in 1.A., systems specified 19.A.1. or 19.A.2. Missile Technology Control Regime (M.TCR): Equipment, software and technology annex M Means information which specific is required for the “development”, “pro M Means information which specific is required for the “development”, “pro M Means information which specific is required for the “development”, “pro M12D2 “Software” which processes post-flight, recorded data, enabling determination of determination enabling data, recorded post-flight, processes which M12D2 “Software”

of dual-use items

is designed for airborne applications and is usable in “missiles”.

equipment or materials specified in 6A, specified 6B or 6C. equipment or materials 6A008, 6A102, c., 6A002, 6A007.b. and in specified “software” or equipment 6D103. or 6D102 6A107, 6A108, 6B108, Note: 6A008 when it in specified equipment for “technology” specifies 6E101 only equipment, materials or “software” specified in 6A, specified 6B, 6C or “software” or 6D. equipment, materials Technical Note: and means systems complete rocket In 6D103 unmanned aerial vehicle ‘missile’ km. systems capable of a range exceeding 300 vehicle position throughout path, its flight designed specially or modified for ‘missiles’. 6E002 “Technology”“production”Technology the according to the General of Note for 6E101 “Technology” according to the General Technology Note for the “use” of 6E001 “Technology” according to the General Technology Note for the “development” of “development” the for Note Technology General the to according 6E001 “Technology” 6D103 “Software” which processes post-flight, recorded data, enabling determination of determination enabling data, recorded post-flight, processes which 6D103 “Software” The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/ Council Regulation (EC) in identified corresponding equipment and components as systems, The 2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit and brokering transfer, exports, of control the for Community regime a 5 up setting 2009 of 2009 May 6E Technology M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 208

developed as Measurement While Drilling (MWD) sensors for use in sensors for use (MWD) Drilling developed as Measurement While operations. service downhole well input. calibration over a period of one year. to a fixed deviation with respect paragraph section 2.214 titled Definitions the Terminology 528-2001 in of agreement closeness ‘The as follows: (gyro, accelerometer) repeatability among repeated measurements of the same variable under the same operating non-operating conditions or conditions when periods occur changes in between measurements’. guidance systems of all types, usable in the systems specified in 1.A., types, in the systems specified guidance 19.A.1. usable systems of all and designed or 19.A.2., specially of the following characteristics, having all components therefor: and ppm; 250 1 than (better) less ‘repeatability’ factor’ a. ‘Scale g. micro 250 1 than (better) less ‘repeatability’ b. ‘Bias’ Note: Item 9.A.3. does not control accelerometers specially designed and Technical Notes: 1. output defined as the accelerometer when is applied. ‘Bias’ no acceleration is 2. change of ratio in output to a change defined as the in the is ‘Scale factor’ 3. The and measurement of ‘bias’ refers to one ‘scale factor’ sigma standard 4. ‘Repeatability’ is defined according to IEEE Standard for Inertial Sensor Missile Technology Control Regime (M.TCR): Equipment, software and technology annex M9A3 Linear accelerometers, designed for use in inertial navigation systems or in or systems navigation inertial in use for designed accelerometers, M9A3 Linear

or CATEGORY 7 — NAVIGATION AND AVIONICS NAVIGATION AND — CATEGORY 7

or of dual-use items

and measurement of only vibration or shock. or vibration only measurement of fixed calibration value over a period of one year; fixed calibration value over a period of one year; fixed calibration of one year; period of one year; function at linear acceleration levels exceeding 100 g; exceeding 100 levels acceleration linear function at and having any of the following: the of and having any a. than 130 of A less (better) micro g “bias” “stability” to with a respect b. to a ppm with respect than 130 (better) less of “stability” factor” A “scale g and having of the following: all than or equal to 100 a. 250 g over a period micro than 1 less (better) of “repeatability” A “bias” a ppm over 250 1 than (better) less of “repeatability” factor” “scale b. A Note: 7A001.a.1. and 7A001.a.2. do not control accelerometers limited to 3. Designed for use in inertial navigation or guidance systems and specified to specified and systems guidance or navigation inertial in use for 3. Designed 1. Specified to function at linear acceleration levels less than or equal to 15 g 15 to equal or than less levels acceleration linear at function to 1. Specified less but g 15 exceeding levels acceleration linear at function to 2. Specified N.B.: SEE ALSO 7A101. ALSO N.B.: SEE N.B.: 7A001.b. For angular see or rotational accelerometers, following: the of any having accelerometers a. Linear 7A001 Accelerometers as follows and specially designed components therefor: components designed specially and follows as 7A001 Accelerometers The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/ Council Regulation (EC) in identified corresponding equipment and components as systems, The 2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit and brokering transfer, exports, of control the for Community regime a 5 up setting 2009 of 2009 May Components and Equipment 7A Systems, M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 209

vibration or shock. independent of input rotation and is expressed as an angular rate. (IEEE STD (IEEE an angular rate. as expressed and is rotation input independent of 528-2001 paragraph 2.56) a exposed to when continuously invariant remain to performance coefficient fixed operating condition. (This definition does not to dynamic refer or servo stability.) (IEEE STD 528-2001 paragraph 2.247) a rated ‘drift rate’ ‘stability’ of less than 0,5 degrees (1 sigma or rms) per hour of less than 0,5 in (1 sigma or rms) degrees ‘stability’ rate’ a rated ‘drift g environment, designed and specially components therefor. a 1 Technical Notes: 1. is defined ‘Drift rate’ as the component of gyro output that is functionally 2. is defined as ‘Stability’ a measure mechanism of the ability a or specific systems or in guidance types, to function at acceleration systems of all specified g, and designed specially components therefor. than 100 levels greater Note: 9.A.5. does not include accelerometers that are designed to measure M9A4 in 1.A., All types of gyros 19.A.1 the systems specified usable in or 19.A.2., with M9A5 navigation use in inertial or gyros of any type, designed for Accelerometers

or or

measured in a 1 g environment over a period of three minutes, and three g environment over a period of in a 1 measured value; to a fixed calibration with respect per square root hour; square root hour; gyros”. mass “spinning control not does Note: 7A002.a.2.b. Note: 7A002.a.1.b. does not control “spinning mass gyros”. mass “spinning control not does Note: 7A002.a.1.b. measured in a 1 g environment over a period of one month, period of and g environment over a with 1 in a measured respect to a fixed value; calibration of the following: than hour, 4 degrees per when (better) of less A “stability” “bias” a. b. 0,0035 than or equal to degree (better) An of less “angle random walk” b. An “angle random walk” of less (better) than or equal to 0,1 degree per degree 0,1 to equal or than (better) less of walk” random “angle b. An following: than 0,5 per hour, degree (better) when of less A “stability” “bias” a. 2. A rate range greater than or equal to 500 degrees per second and having any having and second per degrees 500 to equal or than greater range rate 2. A levels exceeding 100 g. levels exceeding 100 following: the of having any 1. range A of less than 500 rate per second degrees and having any of the components therefor: 7A102. ALSO N.B.: SEE b. Angular or rotational accelerometers, specified to function at linear acceleration linear at function to specified accelerometers, rotational or b. Angular N.B.: 7A001.b. For angular see or rotational accelerometers, a. g Specified to and levels less than function or equal at linear acceleration to 100 7A002 Gyros sensors, having or angular rate any of the following and specially designed

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use in inertial navigation use in inertial

vibration or shock. lisers, automatic pilots and inertial navigation systems. degrees) axes. latitudes of +/– 80 degrees, referenced to local magnetic field; and systems. system accuracy of 3,33 % or less of the “range” (e.g. a ‘CEP’ of 10 km % or or less of the less at “range” (e.g. a ‘CEP’system of accuracy of 3,33 10 km), except as provided Note below 2.A.1. in the those for of 300 a “range” km manned or aircraft; under with a “range” 300 designed missiles for gyros specified in 9.A.4. or 9.A.5., and systems incorporating such equipment, 9.A.5., 9.A.4. incorporating in or and systems gyros specified designed components therefor. and specially Note: 9.A.5. does not include accelerometers that are designed to measure designed components therefor: and specially a. 180 (+/– and having roll 90 degrees) (+/– compensation in pitch tilt Internal at rms degrees 0,5 than (less) better accuracy azimuthal providing of b. Capable c. Designed or modified to be integrated with flight control and navigation Note: Flight control and navigation systems in Item 9.A.8. include gyrostabi systems or in guidance types, to function at acceleration systems of all specified g, and designed specially components therefor. than 100 levels greater M9A6 9.A.5. or 9.A.3. or in specified accelerometers using equipment other or Inertial M9A8 Three axis magnetic heading sensors having all of the following characteristics, following the of all having sensors heading magnetic axis M9A8 Three M2A1d ‘Guidance sets’, usable in the systems specified in 1.A., capable of achieving of capable 1.A., in specified systems the in usable sets’, M2A1d ‘Guidance

Attitude and Heading Reference Systems (AHRSs); Systems Reference Heading and Attitude Gyrocompasses; (IMUs); Units Measurement Inertial (INSs); Systems Navigation Inertial (IRSs); Systems Reference Inertial (IRUs). Units Reference Inertial — which are certified for use on “civil aircraft” by civil aviation authorities by civil aircraft” for use on which “civil are certified of one or more “participating states”. or gyroscopes and to measure changes orientation in velocity in order to determine or maintain heading or position without requiring an external reference once aligned. measurement ‘Inertial equipment or systems’ include: — — — — — a. Global Navigation Satellite Systems (GNSS); Systems Satellite Navigation a. Global Technical Notes: include: and position, provide independently references’ aiding 1. ‘Positional N.B.: SEE ALSO 7A103. ALSO N.B.: SEE Note 2: 7A003 does not control ‘inertial measurement equipment or systems’ b. Specified to function at linear acceleration levels exceeding 100 g. 100 exceeding levels acceleration linear at function to Specified b. M9A5 or gyros of any type, designed for Accelerometers Note 1: measurement equipment incorporate ‘Inertial accelerometers or systems’ 7A003 equipment having measurement or systems’, any of the following: ‘Inertial

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less (better); use of ‘positional aiding references’, and having any of the following accuracies following the and having any of references’, aiding ‘positional use of alignment: normal subsequent to or rate (‘CEP’) Probable’ Error ‘Circular (nm/hr) hour per miles nautical 1. 0,8 2. or less (better); ‘CEP’ % distanced travelled 0,5 Technical Note: 7A003.a.3. typically 7A003.a.2. and 7A003.a.1., in parameters performance The “aircraft”, designed for measurement equipment or systems’ ‘inertial apply to vehicles and These parameters vessels, respectively. result from the utilisation of velocity odometer, altimeter, (e.g., non-positional aiding references specialised performance log). As a consequence, values cannot the specified be readily converted between parameters. these Equipment designed platforms for multiple are evaluated againsteach applicable entry7A003.a.1., 7A003.a.2.,or 7A003.a.3. aiding ‘positional all loss of and providing position after aiding reference’ for a period of up to references’ 4 minutes, having an accuracy of less (better) ‘CEP’; than 10 meters 3. in a 24 hr period; or less (better) mile ‘CEP’ of 1 nautical drift Total Technical Note: 7A003.b. in to systems which measurement equipment refers ‘inertial or systems’ unit single a into built are aiding references’ independent ‘positional and other (i.e., embedded) in order to achieve improved performance. b. “Data-Based Referenced Navigation” (“DBRN”). Navigation” Referenced b. “Data-Based % of the individual containing radius measurements being 50 of the circle made, % probability of being a 50 is within which there circle or the radius of located. a. Designed for “aircraft”, land vehicles or vessels, providing position without the without position providing vessels, or vehicles land “aircraft”, for a. Designed b. or vessels, with an embedded land vehicles ‘positional Designed for “aircraft”, 2. ‘Circular Error Probable’ (‘CEP’) — In a circular normal distribution, the normal distribution, circular a In — (‘CEP’) Probable’ Error 2. ‘Circular

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means of automatically tracking celestial bodies or satellites, and specially bodies or satellites, celestial tracking automatically means of designed components therefor. M9A2 by orientation position or which derive devices compasses and other Gyro-astro

or or systems’ that contain systems’ “spinning mass gyros” as the only type of gyro.

any aiding references; any aiding than “angle random walk” along or equal to 0,1 degree any axis of less (better) per square root hour. accuracy without the use of ‘positional aiding references’ equal to accuracy without or less the use of ‘positional aiding references’ (better) than 0,07 deg (equivalent sec(Lat) to 6 arc minutes rms at 45 degrees latitude); Note: 7A003.d.2. does not control ‘inertial measurement equipment or and a heading accuracy without the use of ‘positional aiding references’ equal references’ aiding ‘positional of use the without heading accuracy and a 45 to minutes rms at 17 arc (equivalent than 0,2 deg sec(Lat) to or less (better) degrees latitude); 20 seconds of arc throughout the specified lifetime of the equipment; 20 throughout seconds lifetime of arc the specified baffles; or heads 1. Optical units. processing 2. Data 1. Performance specified by 7A001 or 7A002 along any axis, without the use of use following: the of and having any one dimension, the without axis, any along 7A002 or 7A001 by specified 1. Performance 2. Being “space-qualified” and providing angular rate measurements having an having measurements rate angular providing and “space-qualified” 2. Being 1. A maximum operating angular rate less (lower) than 500 deg/s and a heading a following: and having the any of determination and deg/s 500 than (lower) less rate angular operating maximum 1. A 2. A maximum operating angular rate equal to or greater (higher) than 500 deg/s 500 than (higher) greater or to equal rate angular operating maximum 2. A N.B.: SEE ALSO 7A104. ALSO N.B.: SEE a. than azimuth accuracy of equal to with a or less (better) specified trackers’ ‘Star follows: 7A004.a. as b. in specified equipment for designed Components specially d. Providing acceleration measurements or angular rate measurements, in more than more in measurements, rate angular or measurements acceleration d. Providing Technical Note: sensors or gyro-astro attitude to as stellar referred are also ‘Star trackers’ compasses. c. North vessels, providing or heading or True land vehicles “aircraft”, Designed for 7A004 ‘Star trackers’ and components therefor, as follows: as therefor, components and trackers’ 7A004 ‘Star

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commercial, civil or ‘Safety of Life’ (e.g. data integrity, flight safety) flight data integrity, (e.g. Life’ of or ‘Safety commercial, civil GNSS services. s; or to GNSS signal/data; to gain access secure services, an environment to function in antenna) steerable electronically antenna or or passive countermeasures. of active ing: 1. m/ Capable of providing navigation at speeds in excess of 600 information governmental or military for modified or designed decryption, 2. Employing steering null (e.g. features employ anti-jam designed to Being specially 3. Note: 11.A.3.b.2. and 11.A.3.b.3. do not control equipment designed for designed equipment control not 11.A.3.b.3. do 11.A.3.b.2. and Note: in the systems specified in 1.A. in the systems specified GLONASS and having specially or Galileo), any of the following characteristics, designed components therefor: a. in 1.A.; or use in systems specified Designed or modified for b. follow the and having any of applications airborne for modified Designed or Technical Note: transmission, Laser radar embody specialised scanning, systems and receiving ranging, for echo direction lasers of utilisation for signal processing techniques and body speed radial location, by targets of and discrimination finding reflection characteristics. guidance systems of all types, usable in the systems specified in 1.A., types, in the systems specified guidance 19.A.1. usable systems of all and designed or 19.A.2., specially of the following characteristics, having all and ppm; 250 components therefor: 1 than (better) less ‘repeatability’ factor’ a. ‘Scale M9A3 Linear accelerometers, designed for use in inertial navigation systems or in or systems navigation inertial in use for designed accelerometers, M9A3 Linear M11A1 Radar and laser radar systems, including altimeters, designed or modified for use for modified or designed altimeters, including systems, radar laser and M11A1 Radar M11A3 Receiving equipment for Global Navigation Satellite Systems (GNSS; e.g. GPS, e.g. (GNSS; Systems Satellite Navigation Global for equipment M11A3 Receiving or and

components designed to filter, switch, or combine signals from multiple from signals combine or switch, filter, to components designed omni-directional antennae that do not implement adaptive antenna tech niques. Controls. Note: 7A005.b. does not control GNSS receiving equipment that only uses Technical Note: purposes For the dynamically generate of 7A005.b antenna ‘adaptive systems’ signal processing in an antenna pattern by nulls in array one or more spatial the time domain or frequency domain. government use to access the ranging code for position and time; ranging code for the access to government use and having any of the following: the and having any of 7A106. ALSO N.B.: SEE management”; a. “Power modulation. key shift phase b. Using inertial navigation systems or in guidance types, inertial systems of all usable in ‘missiles’, components there designed specially and characteristics, following the having all for: 250 g; micro a. than 1 (better) of less A “repeatability” “bias” the following and specially designed the following and specially components therefor: 7A105. ALSO N.B.: SEE N.B.: For equipment specially designed for military use, see Military Goods a. Employing a decryption algorithm specially designed or modified systems’. antenna ‘adaptive for b. Employing 7A006 Airborne altimeters operating at frequencies other than 4,2 to 4,4 GHz inclusive GHz 4,4 to 4,2 than other frequencies at operating altimeters 7A006 Airborne 7A101 other than those specified in Linear accelerometers, 7A001, designed for use in 7A005 Global Navigation Satellite Systems (GNSS) receiving equipment having any of any having equipment receiving (GNSS) Systems Satellite Navigation 7A005 Global

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developed as Measurement While Drilling (MWD) sensors for use in use for sensors (MWD) Drilling While Measurement developed as operations. service downhole well independent of input rotation and is expressed as an angular rate. (IEEE STD (IEEE an angular rate. as expressed and is rotation input independent of 528-2001 paragraph 2.56) a exposed to when continuously invariant remain to performance coefficient fixed operating condition. (This definition does not to dynamic refer or servo stability.) (IEEE STD 528-2001 paragraph 2.247) applied. input. calibration over a period of one year. to a fixed deviation with respect paragraph section 2.214 Definitions titled Terminology 528-2001 the in as repeatability (gyro, follows: accelerometer) closeness of ‘The agreement same among same variable under the the repeated measurements of non-operating periods conditions or when changes in operating conditions occur between measurements’. b. ‘Bias’ ‘repeatability’ less (better) than 1 250 micro g. micro 250 1 than (better) less ‘repeatability’ b. ‘Bias’ Note: Item 9.A.3. does not control accelerometers specially designed and Technical Notes: 1. is defined ‘Drift rate’ as the component of gyro output that is functionally 2. is defined as ‘Stability’ a measure mechanism of the ability a or specific a rated ‘drift rate’ ‘stability’ of less than 0,5 degrees (1 sigma or rms) per hour of less than 0,5 in (1 sigma or rms) degrees ‘stability’ rate’ a rated ‘drift g environment, designed and specially components therefor. a 1 Technical Notes: 1. ‘Bias’ is defined as the accelerometer output when no acceleration is 2. change of defined as the ratio in output to a change is the ‘Scale factor’ in 3. The measurement of ‘bias’ and refers to one ‘scale factor’ sigma standard is defined according Standard to IEEE Sensor 4. ‘Repeatability’ for Inertial M9A4 in 1.A., All types of gyros 19.A.1 the systems specified usable in or 19.A.2., with

Measurement While Drilling (MWD) Sensors downhole for use in (MWD) Drilling well Measurement While service operations. systems capable of a range exceeding 300 km; systems capable of a range exceeding 300 a period of one year; calibration over a fixed standard to deviation with respect systems capable of a range exceeding 300 km. systems capable of a range exceeding 300 when continuously invariant remain to performance coefficient mechanism or STD 528-2001 paragraph operating condition (IEEE a fixed 2.247). exposed to 1. In 7A101 ‘missile’ means complete rocket systems and unmanned aerial vehicle aerial unmanned Technical Notes: and systems rocket complete means ‘missile’ 7A101 1. In 2. In 7A101 the measurement of “bias” and “scale factor” refers to a one sigma g per hour in a 1 than 0,5° of less sigma or rms) (1 ‘stability’ rate” “drift rated designed components environment and specially therefor. Technical Notes: vehicle aerial unmanned and systems rocket complete means ‘missile’ 7A102 1. In of a specific the ability as a measure defined of is In 7A102 ‘stability’ 2. b. A “scale factor” “repeatability” of less (better) than 1 250 ppm; 250 b. than 1 (better) of less “repeatability” A factor” “scale Note: 7A101 does not control accelerometers specially designed and developed as developed and designed specially accelerometers control not does Note: 7A101 7A102 with a in 7A002, gyros, those specified types of other than usable in ‘missiles’, All

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inertial reference unit, or inertial reference inertial navigation system); either periodically or continuously throughout the navi flight (e.g. satellite and radar); and/or Doppler radar altimeter, gation receiver, pilots, designed use in 1.A., or modified for in the systems specified or 19.A.1. or therefor. components designed specially 19.A.2. and 1.A., 19.A.1. or 19.A.2. and capable of providing a navigational accuracy of accuracy navigational a providing of capable 19.A.2. and 19.A.1. or 1.A., 200 m CEP or less. Technical Note: of the following incorporates all typically navigation An ‘integrated system’ system, reference heading components: and attitude an (e.g. device measurement inertial a. An position and/or velocity, update the sensors used to b. One or more external gyros specified in 9.A.4. or 9.A.5., and systems incorporating such equipment, 9.A.5., 9.A.4. incorporating in or and systems gyros specified designed components therefor. and specially M9A1 Integrated flight instrument systems which include gyrostabilisers or automatic or gyrostabilisers include which systems instrument flight M9A1 Integrated M9A7 ‘Integrated navigation systems’, designed or modified for the systems specified in specified systems the for modified or designed systems’, navigation M9A7 ‘Integrated M9A6 9.A.5. or 9.A.3. or in specified accelerometers using equipment other or Inertial

and

in 7A001 where designed such are and specially accelerometers in use sensors for Drilling) While (Measurement developed as MWD operations. services down-hole well inertial navigation systems or in guidance systems of all types, navigation systems or in guidance and systems of all usable in inertial ‘missiles’; specified in 7A002 or 7A102; system, inertial reference unit, or inertial navigation system, inertial reference system); either periodically or continuously throughout navi (e.g., the flight satellite radar); and/or Doppler radar altimeter, gation receiver, pilots, designed or modified for use in ‘missiles’; use in ‘missiles’; for pilots, designed modified or of Equal Probability m Circle of providing of 200 a navigational accuracy (CEP) or less; Note: 7A103.a. does not specify equipment containing accelerometers specified accelerometers containing equipment specify not does Note: 7A103.a. 2. Accelerometers specified in 7A001.a.1. or 7A001.a.2., designed for use in use for designed 7A001.a.2., or 7A001.a.1. in specified 2. Accelerometers systems incorporating such equipment: 1. Accelerometers specified in 7A001.a.3., 7A001.b. or 7A101 or gyros Technical Note: following incorporates the typically navigation An ‘integrated system’ components: 1. An inertial measurement device (e.g., an attitude and heading reference velocity, and/or position the update to used sensors external more or 2. One b. Integrated flight instrument systems which include gyrostabilisers or automatic or gyrostabilisers include which systems instrument flight b. Integrated c. ‘Integrated navigation systems’, designed or modified for ‘missiles’ and capable and ‘missiles’ for modified or designed systems’, navigation c. ‘Integrated 7A003, as follows; and specially designed components therefor: and specially 7A003, follows; as gyros and or as follows, equipment, or other using accelerometers Inertial a. 7A103 Instrumentation, navigation equipment and systems, other than those specified in specified those than other systems, and equipment navigation 7A103 Instrumentation,

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lisers, automatic pilots and inertial navigation systems. degrees) axes. latitudes of +/– 80 degrees, referenced to local magnetic field; and systems. ing: means of automatically tracking celestial bodies or satellites, and specially bodies or satellites, celestial tracking automatically means of designed components therefor. and specially designed components therefor: and specially a. 180 (+/– and having roll 90 degrees) (+/– compensation in pitch tilt Internal at rms degrees 0,5 than (less) better accuracy azimuthal providing of b. Capable c. Designed or modified to be integrated with flight control and navigation c. Integration hardware and software. and hardware 9.D.4. c. Integration Item see “software”, integration N.B. For GLONASS and having specially or Galileo), any of the following characteristics, designed components therefor: a. in 1.A.; or use in systems specified Designed or modified for b. follow the and having any of applications airborne for modified Designed or Note: Flight control and navigation systems in Item 9.A.8. include gyrostabi M9A2 by orientation position or which derive devices compasses and other Gyro-astro M9A8 Three axis magnetic heading sensors having all of the following characteristics, following the of all having sensors heading magnetic axis M9A8 Three M11A3 Receiving equipment for Global Navigation Satellite Systems (GNSS; e.g. GPS, e.g. (GNSS; Systems Satellite Navigation Global for equipment M11A3 Receiving

or izers, automatic pilots and navigation inertial systems. axes; latitude of ± 80 to degrees, reference local magnetic field. sounding rockets specified in 9A104 or unmanned aerial vehicles specified in specified vehicles unmanned aerial 9A104 or in specified sounding rockets 9A112.a.; 9A012 or with flight control and navigation systems, other than those specified in control and navigation systems, other than those specified with flight designed specially and characteristics, following the all 6A006, having components therefor; degrees) 180 (± roll and degrees) 90 (± pitch in compensation tilt 1. Internal at rms degrees 0,5 than (less) better accuracy azimuthal providing of 2. Capable 3. Integration hardware and software; and hardware 3. Integration Note: Flight control Note: and navigation systems in 7A103.d. include gyrostabil GLONASS, or Galileo), other than those specified in 7A005, GLONASS, other than those specified or Galileo), having any of the designed components therefor: and specially following characteristics, a. Designed use or modified for in in space launch 9A004, vehicles specified d. Three axis magnetic heading d. Three axis magnetic sensors, designed to be integrated or modified which derive position or orientation by means of automatically tracking celestial which by position means of automatically or orientation derive designed components therefor. specially and satellites bodies or Technical Note: and means systems unmanned In 7A103 complete rocket ‘missile’ aerial vehicle km. systems capable of a range exceeding 300 7A105 Receiving equipment for Global Navigation Satellite Systems (GNSS; e.g. GPS, e.g. (GNSS; Systems Satellite Navigation Global for equipment 7A105 Receiving 7A104 in 7A004, compasses and other devices, than those specified Gyro-astro

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commercial, civil or ‘Safety of Life’ (e.g. data integrity, flight (e.g. data integrity, Life’ of or ‘Safety commercial, civil safety) GNSS services. services, to gain access to GNSS secure signal/data; or to GNSS signal/data; to gain access secure services, to function in an antenna) environment steerable antenna or electronically or passive countermeasures. of active 1. Capable of providing navigation information at speeds in excess of 600 m/s; 600 of excess in speeds at information navigation providing of 1. Capable governmental or military for modified or designed decryption, 2. Employing steering null (e.g. features anti-jam employ to designed specially 3. Being Note: for designed equipment control not 11.A.3.b.3. do 11.A.3.b.2. and in the systems specified in 1.A. in the systems specified designed or modified for characteristics, finding equipment) or terrain (direction in 1.A. systems specified use in the Technical Note: transmission, Laser radar embody specialised scanning, systems and receiving ranging, for echo direction lasers of utilisation for signal processing techniques and body speed radial location, by targets of and discrimination finding reflection characteristics. M11A2 Passive sensors for determining bearings to specific electromagnetic sources electromagnetic specific to bearings determining for sensors M11A2 Passive M11A1 Radar and laser radar systems, including altimeters, designed or modified for use for modified or designed altimeters, including systems, radar laser and M11A1 Radar or

commercial, civil or ‘Safety of Life’ (e.g., data integrity, flight safety) (e.g., data flight or ‘Safety of Life’ integrity, commercial, civil GNSS services. antenna or electronically steerable antenna) to function in an environment antenna) steerable antenna or electronically or passive countermeasures. of active services, to gain access to GNSS signal/data; to gain access secured services, Note: 7A105.b.2. and 7A105.b.3. do not control equipment designed for designed equipment control not 7A105.b.3. do 7A105.b.2. and Note: 3. Being specially designed to employ anti-jam features (e.g. null steering 1. m/s; Capable of providing navigation at speeds information in excess of 600 2. Employing or governmental decryption, designed military or modified for designed use or modified for in space launch in 9A004 vehicles specified or 9A104. in specified sounding rockets designed (direction finding equipment) or or characteristics, modified terrain for use in 9A004 in space launch vehicles specified or sounding in rockets specified 9A104. b. following: and having the any of applications airborne for modified Designed or 7A115 Passive sensors for determining bearing to specific electromagnetic source electromagnetic specific to bearing determining for sensors 7A115 Passive 7A106 in other than those type, 7A006, specified Altimeters, radar or laser of radar

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a manned aircraft or satellite or in quantities appropriate replacement for quantities or in satellite or a manned aircraft parts for manned aircraft. control systems (including fly-by-wire and fly-by-light systems) designed or systems) and fly-by-light control systems (including fly-by-wire in 1.A. the systems specified modified for km % or or less of the less at “range” (e.g. a ‘CEP’system of accuracy of 3,33 10 km), except as provided Note below 2.A.1. in the those for of 300 a “range” km manned or aircraft; under with a “range” 300 designed missiles for Note: 10.A. of may be exported as part in specified Systems, equipment or valves 10.A.2., and designed or modified to operate in a vibration environment greater than 10 g rms between 20 Hz and 2 kHz. M10A1 Pneumatic, hydraulic, mechanical, electro-optical, or electromechanical flight electromechanical or electro-optical, mechanical, hydraulic, M10A1 Pneumatic, M2A1d ‘Guidance sets’, usable in the systems specified in 1.A., capable of achieving of capable 1.A., in specified systems the in usable sets’, M2A1d ‘Guidance M10A3 Flight control servo valves designed or modified for the systems in 10.A.1. or 10.A.1. in systems the for modified or designed valves servo control M10A3 Flight

a. Terrain contour mapping equipment; mapping contour a. Terrain passive); and active (both equipment sensor b. Imaging equipment interferometer c. Passive systems (including fly-by-wire types); systems (including fly-by-wire 7A116.a. or 7A116.b., and designed or modified to operate in a vibration a in operate 7A116.a. to 7A116.b.,or modified and designed or environment greater than 10 g rms between 20 Hz and 2 kHz. in space launch vehicles specified in 9A004 specified in space launch in or sounding vehicles specified rockets 9A104. a. Hydraulic, mechanical, electro-optical, or electro-mechanical flight control km). km or less at a range of 300 % or less of the range (e.g., a “CEP” of 10 3,33 Note: 7A115 includes sensors for the following equipment: following the for sensors includes Note: 7A115 equipment; control b. Attitude in specified systems the for modified or designed valves servo control c. Flight 1.A. in specified systems the M10A2 for modified or designed equipment control Attitude 7A116 Flight control systems and servo valves, as follows; designed or modified for use 7A117 “Guidance sets”, usable in “missiles” capable of achieving system accuracy of accuracy system achieving of capable “missiles” in usable sets”, 7A117 “Guidance

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mirrors, having the threshold accuracy shown better: mirrors, having the or ppm); (10 1. Scatterometer ppm); (50 2. Reflectometer Tester; Angstroms); (5 3. Profilometer Module (IMU) Unit Measurement 1. Inertial Tester; Fixture; Platform Handling 2. IMU Element Stable Fixture; 3. IMU Balance Platform Station; 4. IMU Test Tuning Station; 5. Gyro Balance Dynamic Station; 6. Gyro Test Station; Run-In/Motor Filling 7. Gyro and Bearings; Evacuation Gyro 8. Gyro for Fixture 9. Centrifuge 10. Accelerometer Axis Align Station; Station; Test 11. Accelerometer 12. Fibre Optic Gyro Coil Winding Machines a. characterise equipment used to following gyro equipment, the laser For equipment: inertial other b. For other than that described in 9.B.2., designed or modified to be used with 9.A. in equipment specified specified in 10.A. Note: Equipment specified in 9.B.1. includes the following: the includes 9.B.1. in specified Note: Equipment Missile Technology Control Regime (M.TCR): Equipment, software and technology annex M2B2 “Production equipment” specially designed for the subsystems specified in 2.A. in specified subsystems the for designed specially equipment” M2B2 “Production M9B1 “Production equipment”, and other test, calibration and alignment equipment, alignment and calibration test, other and equipment”, M9B1 “Production M10B1 Test, calibration, and alignment equipment specially designed for equipment for designed specially equipment alignment and calibration, M10B1 Test,

of dual-use items

tenance Level I’ or ‘Maintenance Level II’. ‘Maintenance Level I’ I’ Level ‘Maintenance II’ Level ‘Maintenance The failure of an inertial navigation unit is detected on the aircraft by indications by aircraft on the detected navigation is unit an inertial of The failure from the Control and Display Unit (CDU) or by the status message from the corresponding sub-system. By following the manufacturer's manual, the cause of Replaceable malfunctioning Line of the level at the may be localised the failure The operator Unit (LRU). then removes the LRU and with a spare. replaces it 2. manufacturer's or that the maintenance workshop to (the sent is LRU The defective of the operator maintenance). responsible II for At the maintenance level to means appropriate various by tested is LRU malfunctioning workshop, the verify and localise Shop the defective Replaceable Assembly (SRA) module removed and an operative SRA is replaced by This failure. the responsible for spare. SRA (or possibly the complete LRU) is then shipped The to the defective of repair or disassembly the include not does II’ Level manufacturer. ‘Maintenance or gyro sensors. controlled accelerometers Technical Notes: 1. Note: 7B001 does not control test, calibration or alignment equipment for ‘Main for equipment alignment or calibration test, control not does Note: 7B001 specified in 7A. 7B001 or alignment equipment, Test, calibration designed specially for equipment The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/ Council Regulation (EC) in identified corresponding equipment and components as systems, The 2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit and brokering transfer, exports, of control the for Community regime a 5 up setting 2009 of 2009 May 7B Test, Inspection and Production Equipment Production and Inspection 7B Test, M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 220

mirrors, having the threshold accuracy shown better: mirrors, having the or ppm); (10 1. Scatterometer ppm); (50 2. Reflectometer Angstroms); (5 3. Profilometer Tester; Module (IMU) Unit Measurement 1. Inertial Tester; Fixture; Platform Handling 2. IMU Element Stable Fixture; 3. IMU Balance Platform Station; 4. IMU Test Tuning Station; 5. Gyro Balance Dynamic Station; 6. Gyro Test Station; Run-In/Motor Filling 7. Gyro and Bearings; Evacuation Gyro 8. Gyro for Fixture 9. Centrifuge 10. Accelerometer Axis Align Station; Station; Test 11. Accelerometer 12. Fibre Optic Gyro Coil Winding Machines. a. characterise equipment used to following gyro equipment, the laser For equipment: inertial other b. For other than that described in 9.B.2., designed or modified to be used with 9.A. in equipment specified following: the includes 9.B.1. in specified Note: Equipment M9B1 “Production equipment”, and other test, calibration and alignment equipment, alignment and calibration test, other and equipment”, M9B1 “Production

(better). follows: 7B102. ALSO N.B.: SEE a. ppm or less (better); of 10 having accuracy a measurement Scatterometers nm (5 angstrom) or less b. having accuracy of 0,5 a Profilometers measurement 7B002 Equipment specially designed to characterize mirrors for ring “laser” gyros, as gyros, “laser” ring for mirrors characterize to designed specially 7B002 Equipment

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mirrors, having the threshold accuracy shown better: mirrors, having the or ppm); (10 1. Scatterometer ppm); (50 2. Reflectometer Angstroms); (5 3. Profilometer Tester; Module (IMU) Unit Measurement 1. Inertial Tester; Fixture; Platform Handling 2. IMU Element Stable Fixture; 3. IMU Balance Platform Station; 4. IMU Test Tuning Station; 5. Gyro Balance Dynamic Station; 6. Gyro Test Station; Run-In/Motor Filling 7. Gyro and Bearings; Evacuation Gyro 8. Gyro for Fixture 9. Centrifuge 10. Accelerometer Axis Align Station; Station; Test 11. Accelerometer 12. Fibre Optic Gyro Coil Winding Machines. a. characterise equipment used to following gyro equipment, the laser For equipment: inertial other b. For other than that described in 9.B.2., designed or modified to be used with 9.A. in equipment specified Note: Equipment specified in 9.B.1. includes the following: the includes 9.B.1. in specified Note: Equipment M2B2 “Production equipment” specially designed for the subsystems specified in 2.A. in specified subsystems the for designed specially equipment” M2B2 “Production M9B1 “Production equipment”, and other test, calibration and alignment equipment, alignment and calibration test, other and equipment”, M9B1 “Production

Gyro tuning test stations; test tuning Gyro stations; balance dynamic Gyro stations; test run-in/motor Gyro stations; fill and evacuation Gyro bearings; gyro for fixtures Centrifuge stations; align axis machines. Accelerometer winding coil gyro optic Fibre — — — — — — — Note: 7B003 includes: Note: 7B003 7B003 Equipment specially designed for the “production” of equipment specified in 7A. in specified equipment of “production” the for designed specially 7B003 Equipment

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mirrors, having the threshold accuracy shown better: mirrors, having the or ppm); (10 1. Scatterometer ppm); (50 2. Reflectometer Angstroms); (5 3. Profilometer Tester; Module (IMU) Unit Measurement 1. Inertial Tester; Platform Fixture; 2. IMU Handling Element Stable 3. IMU Fixture; Balance Platform 4. IMU Station; Test Tuning 5. Gyro Station; Balance Dynamic 6. Gyro Station; Test Run-In/Motor Station; 7. Gyro Filling and Evacuation Bearings; 8. Gyro Gyro for Fixture 9. Centrifuge 10. Accelerometer Axis Align Station; Station; Test 11. Accelerometer 12. Fibre Optic Gyro Coil Winding Machines. a. characterise equipment used to following gyro equipment, the laser For equipment: inertial other b. For other than that described in 9.B.2., designed or modified to be used with 9.A. in equipment specified Note: Equipment specified in 9.B.1. includes the following: the includes 9.B.1. in specified Note: Equipment M9B1 “Production equipment”, and other test, calibration and alignment equipment, alignment and calibration test, other and equipment”, M9B1 “Production a measurement accuracy of 50 ppm less (better). or of 50 accuracy a measurement 7B102 Reflectometers specially designed to characterise mirrors, for “laser” gyros, having gyros, “laser” for mirrors, characterise to designed specially 7B102 Reflectometers

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for the subsystems specified in 2.A in subsystems specified the for

mirrors, having the threshold accuracy shown better: mirrors, having the or ppm); (10 1. Scatterometer ppm); (50 2. Reflectometer Angstroms); (5 Tester; 3. Profilometer Module (IMU) Unit Measurement 1. Inertial Tester; Fixture; Platform Handling 2. IMU Element Stable Fixture; 3. IMU Balance Platform Station; 4. IMU Test Tuning Station; 5. Gyro Balance Dynamic Station; 6. Gyro Test Station; Run-In/Motor Filling 7. Gyro and Bearings; Evacuation Gyro 8. Gyro for Fixture 9. Centrifuge 10. Accelerometer Axis Align Station; Station; Test 11. Accelerometer 12. Fibre Optic Gyro Coil Winding Machines. a. characterise equipment used to following gyro equipment, the laser For equipment: inertial other b. For other than that described in 9.B.2., designed or modified to be used with 9.A. in equipment specified Note: Equipment specified in 9.B.1. includes the following: the includes 9.B.1. in specified Note: Equipment M9B1 “Production equipment”, and other test, calibration and alignment equipment, alignment and calibration test, other and equipment”, M9B1 “Production M2B2* “Production equipment” specially designed for the subsystems specified in 2.A. in specified subsystems the for designed specially equipment” M2B2* “Production

other than that specified in 7B001 specified other than that to 7B003, designed or modified to be used in 7A. with equipment specified b. “Production equipment”, and other test, calibration and alignment equipment, and alignment b. calibration test, “Production equipment”, and other a. “Production facilities” specially designed for equipment specified in 7A117; in specified equipment for designed specially facilities” a. “Production M2B1 designed specially facilities” “Production 7B103 and “production equipment” as follows: “Production facilities”

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the performance or the accuracy of ‘guidance to achieve exceed sets’ specified in 2.A.1.d. aircraft or satellite or in quantities appropriate for or in quantities parts for replacement or satellite aircraft manned aircraft. ities” specified in 2.B.1. specified ities” in 9.A. or 9.B. in 9.A. or ‘guidance sets’ specified in 2.A.1.d. in specified ‘guidance sets’ 9.B. in 9.A. or in 11.A.1., 11.A.2.11.A.4. or specially designed “Software” for the “use” of equipment specified in 11.A.3. Note: 2.D.3. includes “software”, specially designed or modified to enhance to modified designed or specially “software”, Note: 2.D.3. includes 10.B. in 10.A. or Note: in 10.D.1. “Software” specified may be exported as part of a manned Missile Technology Control Regime (M.TCR): Equipment, software and technology annex M2D the “use” of “production designed specially or modified for facil “Software” M9D1 of equipment the “use” specified designed modified for specially or “Software” M9D1 of equipment the “use” specified designed modified for specially or “Software” M2D3 designed operation or maintenance of specially or modified for the “Software”, M10D1 of equipment the “use” specified designed modified for specially or “Software” M11D1&2 of equipment the “use” specified designed modified for specially or “Software”

transit of dual-use items

‘AHRS’.

7A001 to 7A006, 7A101 to 7A106, 7A115, 7A116.a., 7A116.b., 7B001, 7B002, 7A006, 7A101 to 7A001 to 7B103. or 7B003, 7B102 Note: 7D002 does not control “source code” for the “use” of gimballed equipment, including inertial equipment not specified in 7A003 7A004, in or or specified not equipment equipment, including inertial Attitude and Systems (‘AHRS’). Heading Reference Technical Note: ‘AHRS’ generally differ from Inertial Navigation Systems (INS) in that an ‘AHRS’ provides attitude and heading information and normally does not and with an position information associated acceleration, velocity provide the INS. 7D101 designed the “use” of equipment specially in or modified for “Software” specified 7D002 navigation operation or maintenance of any “Source code”for the inertial 2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and brokering transfer, exports, of control the for Community regime a up 5 2009 setting 2009 of May The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/ Council Regulation (EC) in identified The corresponding systems, equipment and components as 7D Software M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 225

Note: A common form of integration “software” employs Kalman filtering. Kalman employs “software” integration of form common Note: A the systems specified in 1.A. in 2.A the subsystems the systems specified or 20.A. or specified Technical Note: aerodynamic and particular the in thermodynamic The modelling includes analysis of the systems. systems’ specified in 9.A.7. systems’ specified duction” or “use” of a product. The may information of take the “technical form assistance”. data” or “technical Missile Technology Control Regime (M.TCR): Equipment, software and technology annex M Means information which specific is required for the “development”, “pro M9D2 Integration “software” for the equipment specified in 9.A.1. in specified equipment the for “software” M9D2 Integration M9D4 Integration “software”, designed or modified for the ‘integrated navigation ‘integrated the for modified or designed “software”, M9D4 Integration M16D1 “Software” specially designed for modelling, simulation, or design integration of integration design or simulation, modelling, for designed specially M16D1 “Software” M9D3* Integration “software” specially designed for the equipment specified in 9.A.6. in specified equipment the for designed specially “software” M9D3* Integration

of dual-use items

specified in 7A005.a. specially designed hardware specified in 4A102.

7A103.c. 7A003 or 7A103.a. 7A003 or equipment or “software”, specified in 7A, 7B, specified 7D001, equipment or “software”, 7D002, 7D003, 7D005 and 7D103.7D101 to specified in 7A117 design or for their integration with the space launch vehicles specified in 9A004 or sounding rockets in specified 9A104. Note: 7E001 includes key management “technology” exclusively for equipment c. Integration “software” designed or modified for the equipment specified in specified equipment the for modified or designed “software” c. Integration filtering. Kalman employs “software” integration of form common Note: A Note: “Software” specified in 7D103 remains controlled when combined with combined when controlled 7D103 remains in specified Note: “Software” a. Integration “software” for the equipment specified in 7A103.b.; in specified equipment the for “software” a. Integration b. Integration “software” specially designed for the equipment specified in 7E001 “Technology” according to the General Technology Note for the “development” of “development” the for Note Technology General the to according 7E001 “Technology” 7D103 designed specially for modelling of the “guidance or simulation “Software” sets” 7D102 Integration “software” as follows: as “software” 7D102 Integration The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/ Council Regulation (EC) in identified corresponding equipment and components as systems, The 2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit and brokering transfer, exports, of control the for Community regime a 5 up setting 2009 of 2009 May 7E Technology M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 226

of a manned aircraft, satellite, land vehicle, marine/submarine or land of a manned vehicle, vessel aircraft, satellite, appropriatereplacement geophysical survey equipment or in quantities for parts for such applications. duction” or “use” of a product. The may information of take the “technical form assistance”. data” or “technical opment”, in 2.A., “production” specified or “use” of equipment or “software” 2.D. 2.B. or opment”, in 9.A., “production” specified or “use” of equipment or “software” 9.D. 9.B. or Note: Equipment in 9.A. or 9.D. or “software” specified may be exported as part M Means information which specific is required for the “development”, “pro M2E1 “Technology”, in accordance with the General Technology Note, for the “devel the for Note, Technology General the with accordance in M2E1 “Technology”, M9E1 “Technology”, in accordance with the General Technology Note, for the “devel the for Note, Technology General the with accordance in M9E1 “Technology”,

calibration, removal or replacement of damaged LRUs and or unserviceable or ‘Main I’ ‘Maintenance Level as described in aircraft” “civil of a SRAs II’. tenance Level conventional air data probes; data conventional air actuator package) specially designed for “primary flight control”; “active flight control systems”; databases, that provide a positioning accuracy equal to or less (better) than (better) less equal to or provide a positioning accuracy databases, that miles; 0,4 nautical 2. Air data systems based on surface static data only, i.e., which dispense with dispense used; which 1. Not i.e., only, data static surface on based systems data 2. Air “aircraft”; for displays dimensional 3. Three used; 4. Not integrated and electrohydrostatic electromechanical, (i.e., actuators 5. Electric 6. “Flight control optical sensor array” specially designed for implementing 7. “DBRN” systems designed to navigate underwater, using sonar or gravity or sonar using underwater, navigate to designed systems 7. “DBRN” equipment specified in 7A or 7B. 7A or in equipment specified a. “Technology” for the “development” or “production” of any of the following: bishing in 7A001 or overhaul of equipment specified to 7A004. 7B001. to Notes Technical N.B.: See Note: 7E003 does not control maintenance “technology” directly associated with associated directly “technology” maintenance control not does Note: 7E003 7E004 Other “technology” as follows: as “technology” 7E004 Other 7E002 “Technology”“production”Technology the according to the General of Note for 7E003 “Technology” Technology according to refur the General Note for the repair,

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and lifting control surfaces, designed or modified for the systems specified in 1.A. in specified systems the for modified designed or surfaces, control and lifting of regime throughout the flight or 19.A.2.,aerodynamic performance to optimise vehicle. an unmanned aerial M10E1 Design “technology” for integration of air vehicle fuselage, propulsion system propulsion fuselage, vehicle air of integration for “technology” M10E1 Design

maintenance. effects through comparison of redundant data sources, or off-line pre- failures. anticipated to planned responses navigation and propulsion control data, into a digital flight management flight digital a data, into navigation and propulsion control path system for “flight optimisation”; a. “Development” “technology” for integration of digital flight control, “Development” “technology”digital flight for integration of a. moment controls to mitigate “active flight control system” degradations and degradations system” control flight “active moment controls to mitigate failures; state, transferring flight control data, or state, transferring commanding actuator movement, control systems”; flight “active systems” “fly-by-light for “required” impending preemptively mitigate degradation and of components failures control system”; flight within an “active Note: 7E004.b.3. does notNote: control algorithms for purpose of off-line Note: 7E004.b.4. fault elimination of the does not control algorithms for flight”; control of “total management system for flight into a digital 4. Real-time algorithms to identify component failures and reconfigure force and force reconfigure and failures component identify to algorithms 4. Real-time (including “fly-by-wire systems” or “fly-by-light systems”): systems”): “fly-by-light or systems” (including “fly-by-wire component control flight or aircraft sensing for “technology” 1. Photonic-based used; 2. Not 3. and component to predict to analyze sensor information algorithms Real-time 5. Integration of digital flight control, navigation and propulsion control data, control propulsion and navigation control, flight digital of 5. Integration b. “Development” “technology”, as follows, for “active flight control systems” control: not does Note: 7E004.b.5.

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and Note: 7E004.b.7.b.3. does not control autopilots. control not does Note: 7E004.b.7.b.3. than or landing, 18 greater off degrees angle at of attack, 15 degrees side rate; roll 90 degrees/second or yaw rate, or pitch 15 degrees/second slip, Technical Note: ‘Abnormal changes in aircraft state’ include in-flight structural damage, of engine thrust, disabled loss control surface, or destabilizing shifts in cargo load. in the design flight envelope, that would lose recoverable control if not if control envelope, design that would in the flight recoverable lose corrected within 0,5 seconds; state’; aircraft changes in integrated solely for VOR, DME, ILS or MLS navigation or integrated solely approaches. 40 Hz or greater; 4. Enables aircraft to have stable controlled flight, other than during take- during than other flight, controlled stable have to aircraft 4. Enables 3. Preforms the functions specified in 7E004.b.5.; in specified functions the 3. Preforms Technical Note: flight control systems” that to functions of “active ‘Inner-loop’ refers controls. stability automate airframe point any at measured airframe, unstable aerodynamically an 1. Corrects ‘abnormal for compensating while axes more or two in controls 2. Couples b. “Development” “technology” flight instrument systems for “aircraft” b. wire systems” having wire systems” all of the following: of rates loop closure requiring controls stability airframe a. ‘Inner-loop’ b. Having any of the following: the of any b. Having 6. Not used; 6. Not 7. for “fly-by- requirements for deriving the functional “required” “Technology”

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duction” or “use” of a product. The may information of take the “technical form assistance”. data” or “technical M Means information which specific is required for the “development”, “pro

–9 and

aw controls; computer elements and utilities (e.g., input signal acquisition, and computer elements utilities program transmission, computer and data loading, output signal task scheduling mechanisms) not providing a specific test, built-in flight control system function. functions of at least two of the following into one controlling element: functions of at least controls; a. Collective controls; b. Cyclic c. Y control systems”; systems using individual blade control. Note: 7E004.b. does not control technology associated with common the combine which controllers, fly-by-light or fly-by-wire 1. Multi-axis directional circulation-controlled or anti-torque 2. “Circulation-controlled 3. Rotor blades incorporating “variable geometry airfoils”, for use in any two individual faults within the “fly-by-wire system”; “fly-by-wire the within faults individual any two failures per flight hour; b. than 1 being × 10 less (better) Probability of loss of control the aircraft c. systems, follows: the “development”as for of helicopter “Technology” wire systems” to achieve all of the following: to achieve wire systems” all a. consecutive sequence event of a of in the No the aircraft loss of control 8. “fly-by- for requirements deriving the functional for “required” “Technology” equipment in 7A001 specified to 7A006, 7A101 to 7A106, 7A115 to 7A117, 7D103. to 7B103, 7D101 7B001, 7B002, 7B003, 7B102, 7E101 “Technology” according to the General Technology Note for the “use” of

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or less (at maximum (at or less

–1 h

–1

excluding civil certified engines with a ‘maximum thrust value’ greater value’ thrust ‘maximum a with engines certified excluding civil and than 8,89 un-installed); kN (achieved continuous power at sea level static conditions using the ICAO standard ICAO the using conditions static level sea at continuous power atmosphere); subsystems; 1. ‘Maximum thrust value’ greater than N 400 (achieved un-installed) 2. Specific fuel consumption kg of N 0,15 Technical Note: In 3.A.1.a.1., ‘maximum thrust value’ is the manufacturer's demonstrated type certified maximum The civil thrust for the engine type un-installed. Electromagnetic Pulse (EMP) and (EMI) hazards Interference Electromagnetic sources, as follows: from external systems; shielding for “technology” a. Design and circuits electrical hardened of configuration the for “technology” b. Design above. the for criteria hardening of determination for “technology” c. Design propulsion data into a flight management system, designed or modified for the for modified designed or system, management flight a into propulsion data in 1.A. systems specified or 19.A.1., system trajectory. of rocket for optimisation a. Engines having both of the following characteristics: following the of both having a. Engines Missile Technology Control Regime (M.TCR): Equipment, software and technology annex M3A1 Turbojet and turbofan engines, as follows: as engines, turbofan and M3A1 Turbojet M11E1 Design “technology” for protection of avionics and electrical subsystems against subsystems electrical and avionics of protection for “technology” M11E1 Design M10E2 Design “technology” for integration of the flight control, guidance, and guidance, control, flight the of integration for “technology” M10E2 Design

CATEGORY 9 — AEROSPACE AND PROPULSION AEROSPACE AND — CATEGORY 9

and of dual-use items

the following has been issued by civil aviation authorities of one or the following has been issued by civil engine specific with this aircraft for the states” more “participating type: pating states”; or b. Intended to power non-military manned aircraft for which any of any which for aircraft manned non-military power to b. Intended the following: “partici more or one of authorities aviation civil the by a. Certified subsystems; 7E102.b. 9E003.i.; Note 1: 9A001.a. of does all not control aero gas turbine engines which meet tromagnetic pulse (EMP) and electromagnetic interference (EMI) hazards, from (EMI) tromagnetic pulse (EMP) and interference electromagnetic external sources, as follows: systems; shielding for “technology” a. Design and circuits electrical hardened of configuration the for “technology” b. Design and 7E102.a. of criteria hardening of determination the for “technology” c. Design data into a flight management system for optimization of rocket system trajectory. of rocket optimization management system for data into a flight 9A101. ALSO N.B.: SEE a. Incorporating any of the “technologies” specified in 9E003.a., 9E003.h. or 7E102 “Technology” for protection of avionics and electrical subsystems against elec against subsystems electrical and avionics of protection for 7E102 “Technology” 7E104 “Technology” for the integration of the flight control, guidance, and propulsion and guidance, control, flight the of integration the for 7E104 “Technology” 9A001 Aero gas turbine engines having any of the following: the of any having engines turbine gas 9A001 Aero The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/ Council Regulation (EC) in identified corresponding equipment and components as systems, The 2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit and brokering transfer, exports, of control the for Community regime a 5 up setting 2009 of 2009 May Components and Equipment 9A Systems, M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 231

or in quantities appropriate for replacement parts for a manned aircraft. thrust value will be equal thrust value will than to or less the manufacturer's demonstrated type. engine the for maximum thrust consumption. fuel or specific of thrust regardless vehicles, and sounding rockets) capable of delivering at least a 500 kg vehicles, and a 500 sounding least capable of delivering at rockets) km. 300 “payload”of at least to a “range” b. Engines designed in 1.A. or modified for systems specified or 19.A.2., b. Note: in 3.A.1. Engines may be exported as part of a manned specified aircraft vehicles, and sounding in 1.A.1., not specified “range” rockets), capable of a km. than 300 equal to or greater M1A1 Complete rocket systems (including ballistic missile systems, space launch space systems, missile ballistic (including systems rocket M1A1 Complete M19A1 Complete rocket systems (including ballistic missile systems, space launch space systems, missile ballistic (including systems rocket M19A1 Complete

handling’ includes bus data management, storage, and processing. Aviation Organisation (ICAO). Auxiliary Power approved Units (APUs) aviation by the civil authority in a “participating state”. 2. An equivalent document recognized by the International Civil 1. A civil type certificate; type civil 1. A Note: For the purpose of 9A004.e.1., ‘command and telemetry data telemetry and ‘command 9A004.e.1., of purpose the Note: For 3A002.g., 5A001.a.1., 5A001.b.3., 5A002.a.5., 5A002.a.9., 6A002.a.1., 6A002.a.2., 6A002.b., 6A002.d., 6A003.b., 6A004.c., 6A004.e., 6A008.d., 9A010.c.; or 6A008.e., 6A008.k., 6A008.l. functions: following the any of handling’; data telemetry and 1. ‘Command Note 2: 9A001.a. engines designed for aero gas turbine does not control 2: Note thirty minutes. “spacecraft” on-board systems or equipment, and terrestrial equipment, as follows: equipment, as equipment, and on-board systems or terrestrial “spacecraft” 9A104. ALSO N.B.: SEE vehicles; launch a. Space b. “Spacecraft”; buses”; c. “Spacecraft d. “Spacecraft payloads” incorporating items specified in 3A001.b.1.a.4., having and “spacecraft” for designed specially equipment, or systems e. On-board b. Designed to power an aircraft to cruise at Mach 1 or higher, for more than at Mach 1 or higher, b. for to cruise Designed to power an aircraft 9A004 payloads”, buses”, “spacecraft “spacecraft “spacecraft”, vehicles, Space launch

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Ns;

6 2.A.1.c.2., designed or modified for use on satellites, may be treated as treated be may satellites, on use for modified or 2.A.1.c.2., designed and statements end-use to subject exported is subsystem the if Category II, appropriate quantity limits excepted end-use stated above, for the when than 1kN. greater not having a vacuum thrust capacity equal to or greater than 1,1 × 10 capacity equal to than or greater 1,1 designed into or modified to be a liquid propellant or gel integrated, than greater or to equal capacity impulse total a has which propulsion system 1,1 × 10 1. Solid propellant rocket motors or hybrid rocket motors having a total impulse 2. Liquid propellant rocket engines gel propellant rocket motors integrated, or or Note: in Liquid propellant engines specified apogee engines or station-keeping M2A1a in 1.A.; specified stages usable in the systems Individual rocket M2A1c Rocket in 1.A., propulsion specified as follows; subsystems, usable in the systems

sensing and actuation to determine and control the position and position the and control determine to and actuation sensing a “spacecraft”. orientation of payload data management, storage, and processing. Goods Controls. Note: For the purpose of 9A004.e.3., ‘attitude and orbit control’ includes control’ orbit and ‘attitude 9A004.e.3., of purpose the Note: For N.B.: For equipment specially designed for military use, see Military see use, military for designed specially equipment N.B.: For Note: For the purpose of 9A004.e.2., ‘payload data handling’ includes handling’ data ‘payload 9A004.e.2., of purpose the Note: For 3. ‘Attitude and orbit control’; orbit and 3. ‘Attitude 2. ‘Payload data handling’; data 2. ‘Payload 1. Telemetry and telecommand equipment; telecommand and 1. Telemetry 2. Simulators. specified in 9A006. 9A119. AND 9A105 ALSO N.B.: SEE f. Terrestrial equipment, specially designed for “spacecraft” as follows: as “spacecraft” for designed specially equipment, f. Terrestrial 9A005 Liquid propulsion rocket systems containing any of the systems or components,

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Ns, but less than Ns, but less

5 Ns;

6 Ns, but less than 1,1 × 10 than 1,1 Ns, but less

5 Ns;

6 impulse capacity equal to or greater than 8,41 × 10 than 8,41 impulse capacity equal to or greater or designed or modified to be integrated, into a liquid propellant or gel into a liquid propellant or designed modified to be integrated, or equal to or propellant propulsion capacity impulse system which has a total × 10 greater than 8,41 1,1 × 10 19.A.; specified in 19.A.1., as follows: 1. Solid propellant rocket motors or hybrid rocket motors having a total 2. Liquid propellant rocket engines or gel propellant rocket motors integrated, 4.C. in 1.A.1. used in the systems specified or other liquid propellants a. Individual rocket stages, not specified in 2.A.1., usable in systems specified in specified systems in usable 2.A.1., in specified not stages, rocket a. Individual b. Rocket propulsion subsystems, in 2.A.1., not specified usable in the systems M3A8 Liquid propellant tanks specially designed for the propellants controlled in Item in controlled propellants the for designed specially tanks propellant M3A8 Liquid M20A1 Complete subsystems as follows: as subsystems M20A1 Complete

systems, specially designed for use in space vehicles and capable of restricting use in space vehicles and of restricting designed capable systems, specially for year; per % than 30 to less losses cryogenic fluid capable of sustained “aircraft” for °C) or less of 100 K (–173 temperatures speeds flight at exceeding Mach 3, launch vehicles or “spacecraft”; associated gas or expander generator cycle turbine drive systems; b. Cryogenic containers or closed-cycle refrigeration systems, capable of providing of capable systems, refrigeration closed-cycle or containers b. Cryogenic as follows: 9A120. AND 9A108 9A106, ALSO N.B.: SEE a. flightweight dewars, cryogenic heat pipes or cryogenic Cryogenic refrigerators, systems; transfer or storage hydrogen c. Slush their or components pump pumps, turbo MPa) 17,5 (exceeding pressure d. High 9A006 Systems and components, specially designed for liquid rocket propulsion systems, propulsion rocket liquid for designed specially components, and 9A006 Systems

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opellant rocket engines usable in opellant rocket

minute, at an absolute pressure equal to or greater than 7 MPa, have that ms. than 100 less of response time an actuator 8 000 rpm at the maximum 7 MPa. than operating greater or equal to mode or with discharge pressures maximum operating mode. the 000 rpm at than 8 or greater following: a. per than 24 litres or greater equal to rates flow designed for Servo valves b. Pumps, for liquid propellants, with shaft speeds equal to or greater than c. Gas turbines, for liquid propellant turbopumps, with shaft speeds equal to satellite. specially designed components therefor, usable in the systems specified in 1.A., designed components specially usable in the systems specified therefor, g rms designed than 10 or modified to operate in vibration environments greater Hz and 2 kHz. between 20 the subsystems specified in 2.A.1.c.2. the subsystems specified or 20.A.1.b.2. Notes: 3.A.5. pumps in are the valves, and 1. The only servo gas turbines specified 2. Systems and components in 3.A.5. may be exported as part of a specified

M3A5 M3A5 Liquid, slurry and gel propellant (including oxidisers) control systems, and systems, control oxidisers) (including propellant gel and slurry M3A5 Liquid, M3A8 M3A10 and tensile strengths exceeding 48 strengths and tensile

3 or smaller for non-circular orifices) and orifices) non-circular for or smaller

2 cm

–3 specially designed for liquid rocket engines; diameter (an area of 1,14 × 10 diameter (an area of 1,14 g/cm exceeding 1,4 densities cones, with positive expulsion (i.e., with flexible bladders); positive expulsion with flexible (i.e., MPa. g. Liquid propellant injectors with individual orifices of 0,381 mm or smaller in mm or smaller g. of 0,381 with individual orifices Liquid propellant injectors carbon-carbon exit or one-piece chambers carbon-carbon thrust One-piece h. e. High-pressure (exceeding 10,6 MPa) thrust chambers and nozzles therefor; nozzles and chambers thrust MPa) 10,6 (exceeding e. High-pressure pr liquid M3A10 for nozzles and chambers Combustion or containment capillary of principle the using systems storage f. Propellant

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Ns;

6 in 2.A.1.c.2., may be treated designed or modified for use on satellites, end-use to exported subject subsystem is the if as Category II, appropriate statements and quantity limits for the excepted end-use stated above, when having a vacuum thrust not greater than 1kN. or designed or modified to be integrated, into a liquid propellant or gel into a liquid propellant or designed modified to be integrated, or equal to or propellant propulsion capacity impulse system which has a total × 10 greater than 1,1 materials; capacity materials; × 10 than 1,1 equal to or greater impulse capacity Note: Liquid propellant apogee engines or station-keeping engines specified engines station-keeping or engines apogee propellant Note: Liquid 2. Liquid propellant rocket engines or gel propellant rocket motors integrated, systems specified in 1.A., systems specified as follows, except provided in the Note below payloads: non-weapon for designed those 2.A.1. for 1. Heat shields, and or ablative of ceramic components fabricated therefor, heat high light-weight, of fabricated therefor, components and sinks 2. Heat vehicles; re-entry for designed specially equipment 3. Electronic follows; 1. Solid propellant rocket motors or hybrid rocket motors having a total a. in 1.A.; specified stages usable in the systems Individual rocket the in usable therefor, modified or designed equipment and vehicles, b. Re-entry as 1.A., in specified systems the in usable subsystems, propulsion c. Rocket M2A1 in 1.A., Complete subsystems specified usable in the systems as follows:

to provide a ‘strong mechanical bond’ or a barrier to chemical migration chemical to barrier bond’or a mechanical to provide a ‘strong insulation material. and case between the solid propellant ambient sea level conditions for an adjusted chamber pressure of 7 MPa; an conditions adjusted chamber pressure for ambient sea level 86 %; Technical Note: ‘Strong mechanical bond’means bond more than or strength equal to propellant strength. e. Insulation and propellant bonding systems, using direct-bonded motor designs motor direct-bonded using systems, bonding propellant and e. Insulation N.B.: SEE ALSO 9A107 AND 9A119. AND 9A107 ALSO N.B.: SEE MNs; 1,1 exceeding capacity impulse a. Total b. impulse of 2,4 Specific kNs/kg or more, when the nozzle flow is expanded to % and propellant solid loadings exceeding c. exceeding 88 Stage mass fractions 9A008; in specified d. Components 9A007 Solid rocket propulsion systems having any of the following: the of any having systems propulsion rocket 9A007 Solid

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vehicle's position and velocity (i.e. navigation) with that of computing and sending to correct the control systems commands flight to the vehicle's trajectory. range, which 50 in a specific of target, at % at the centred circle radius of the the payloads impact. system accuracy of 3,33 % or less of the “range” (e.g. a ‘CEP’ of 10 km % or less of (e.g. or less the “range” a ‘CEP’system accuracy of 3,33 of 10 km), except as provided in the Note below of 300 at a “range” 2.A.1. for those km or manned aircraft; under 300 with a “range” designed for missiles Technical Notes: 1. A ‘guidance set’ integrates the process of measuring and computing a 2. is a measure of accuracy, of equal defined as the probability) (circle ‘CEP’ as provided in the Note below 2.A.1. systems that for those designed rocket for 1.A.; in specified systems of capability “range”/“payload” the exceed do not Technical Note: control: vector thrust achieving methods of following the 2.A.1.e. includes nozzle; a. Flexible injection; gas secondary or b. Fluid nozzle; or engine c. Movable probes); or vanes (jet stream gas exhaust of d. Deflection e. Use of thrust tabs. d. ‘Guidance sets’, usable in the systems specified in 1.A., capable of achieving of capable 1.A., in specified systems the in usable sets’, d. ‘Guidance e. in 1.A., Thrust vector control subsystems, usable in the systems specified except

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Ns;

treated as Category II if the subsystem is exported subject to end-use the subsystem is if treated as Category II statements and appropriatequantity limits for the excepted end-use stated above. eapon or warhead safing, arming, fuzing, and firing mechanisms, usable in the mechanisms, usable fuzing, and firing arming, safing, warhead eapon or systems specified in 1.A., specified except as provided systems in the Note below 2.A.1. those for 1.A. in specified those than other systems designed for f. W Note: to 3.C.2. Refer for ‘insulation’ material in bulk or sheet form. systems specified in 1.A. systems specified or 19.A.1. Technical Note: In 3.A.3. intended to be applied components ‘insulation’ to the a rocket motor, of case closures, includes cured or semi-cured case, nozzle inlets, i.e. the compounded rubber components comprising sheet stock containing an insulating or refractory material. It may also be incorporated boots as stress relief or flaps. Note: The exceptions in 2.A.1.b., 2.A.1.d., 2.A.1.e. and 2.A.1.f. above may be Solid rocket motors or hybrid motors having propellant rocket impulse a total × 10 than capacity equal 1,1 to or greater

M3A3 Rocket motor cases, ‘insulation’ components and nozzles therefor, usable in the in usable therefor, nozzles and components ‘insulation’ cases, motor M3A3 Rocket M2A1c1

Technical Note: ‘Strong mechanical bond’means bond more than or strength equal to propellant strength. mechanical bond’ or a barrier to chemical migration between the to chemical migration mechanical bond’solid or a barrier insulation material; propellant and case N.B.: SEE ALSO 9A108. ALSO N.B.: SEE ‘strong a provide to liners using systems, bonding propellant and a. Insulation 9A008 Components specially designed for solid rocket propulsion systems, as follows: as systems, propulsion rocket solid for designed specially 9A008 Components

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2.A.1.c.1. or specially designed for subsystems specified in 20.A.1.b.1. in specified subsystems for designed specially 2.A.1.c.1. or Technical Note: In 3.C.1. ‘interior lining’ suited for the bond between interface the solid polymer based liquid usually a is liner or insulating propellant and case the HTPB or other e.g. carbon or insulating materials filled dispersion of refractory polymer with added interior. a case be sprayed or screeded over curing agents to specified in 2.A.1.c.1. or specially designed for subsystems in specified 20.A.1.b.1. Technical Note: In 3.C.2. intended ‘insulation’ to be applied to the components of a rocket motor, case closures, includes cured or semi-cured case, nozzle inlets, i.e. the compounded rubber sheet stock containing an insulating or material. refractory It may also be incorporated as stress relief boots or flaps specified in 3.A.3. Technical Note: control: vector thrust achieving of methods following the 2.A.1.e. includes nozzle; a. Flexible injection; gas secondary or b. Fluid nozzle; or engine c. Movable probes); or vanes (jet stream gas exhaust of d. Deflection tabs. thrust of e. Use as provided in the Note below 2.A.1. for those designed for rocket systems that rocket Note below those designed for 2.A.1. as provided in the for 1.A.; in specified systems of capability “range”/“payload” the exceed do not M3C1 ‘Interior lining’ usable for rocket motor cases in the subsystems specified in specified subsystems the in cases motor rocket for usable lining’ M3C1 ‘Interior M3C2 motor cases in the subsystems rocket in bulk usable for form material ‘Insulation’ M2A1e Thrust vector control subsystems, in 1.A., usable in the systems specified except

or or more

2 having ‘structural efficiency ratios (PV/W)’ exceeding 25 km; 25 exceeding (PV/W)’ ratios efficiency having ‘structural mm/s; than 0,075 capable of any of the following: 5°; ± exceeding movement 1. Omni-axial more; or 20°/s of rotations vector 2. Angular 3. Angular vector accelerations of 40°/s of accelerations vector 3. Angular Technical Note: by the multiplied the burst pressure (P) is ratio (PV/W)’ ‘Structural efficiency vessel volume (V) divided by the total pressure weight vessel (W). c. Nozzles with thrust levels exceeding 45 kN or nozzle throat erosion rates of less b. Filament-wound “composite” motor cases exceeding 0,61 m in diameter or m in diameter cases exceeding 0,61 Filament-wound motor “composite” b. d. Movable nozzle or secondary fluid injection thrust vector control systems,

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6 Ns, but less than 1,1 × 10 than 1,1 Ns, but less

Ns;

Ns; 6

Ns, but less than 1,1 × 10 than 1,1 Ns, but less

5 capacity equal to or greater than 8,41 × 10 than 8,41 capacity equal to or greater designed into or modified to be a liquid propellant or gel integrated, than greater or to equal capacity impulse total a has which propulsion system 8,41 × 10 use in the systems specified in 1.A., 19.A.1. use in the systems specified or 19.A.2. and the subsystems specified in 2.A. or 20.A. capacity equal to or greater than 1,1 × 10 than 1,1 capacity equal to or greater specified in 19.A.1., as follows: 1. Solid propellant rocket motors or hybrid rocket motors having a total impulse 2. Liquid propellant rocket engines gel propellant rocket motors integrated, or or M6A1 Composite structures, laminates, and manufactures thereof, specially designed for designed specially thereof, manufactures and laminates, structures, M6A1 Composite M2A1c1 Solid rocket motors or hybrid motors having propellant rocket impulse a total M20A1b Rocket propulsion subsystems, in 2.A.1., not specified usable in the systems

specified in 1C0010.e. and resins specified in 1C008 or 1C009.b.; 1C007; in specified a. Materials launch vehicles manufactured using any of the following: the using any of manufactured launch vehicles materials” consisting of “fibrous or filamentary “Composite” materials 1. 2. by any “composites” reinforced of the following: Metal “matrix” b. Thrust levels exceeding 220 kN in vacuum exit conditions. exit vacuum in kN 220 exceeding levels b. Thrust vehicle propulsion systems or “spacecraft”, as follows: vehicle propulsion systems or “spacecraft”, 9A110. AND 1A002 ALSO N.B.: SEE designed for and specially kg a. exceeding 10 each Components and structures, N.B.: SEE ALSO 9A109 AND 9A119. AND 9A109 ALSO N.B.: SEE MNs; 1,1 exceeding capacity impulse a. Total 9A010 Specially designed components, systems and structures, for launch vehicles, launch vehicles, launch for structures, and systems components, designed 9A010 Specially 9A009 Hybrid rocket propulsion systems having any of the following: the of any having systems propulsion rocket 9A009 Hybrid

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use in the systems specified in 1.A., 19.A.1. use in the systems specified or 19.A.2. and the subsystems specified in 2.A. or 20.A. systems the in usable components therefor, designed specially combustion, and specified in 1.A. or 19.A.2. use in the systems specified in 1.A., 19.A.1. use in the systems specified or 19.A.2. and the subsystems specified in 2.A. or 20.A. Technical Note: 3.A.2., are the engines engines’ In Item that employ two ‘combined cycle or more turboprop, following of engines: gas-turbine engine of the (turbojet, types cycles turbofan and turboshaft), ramjet, scramjet, pulse jet, detonation engine, and rocket motor (liquid/solid-propellant hybrid). M6A1 Composite structures, laminates, and manufactures thereof, specially designed for designed specially thereof, manufactures and laminates, structures, regulate M6A1 Composite to devices including engines’, cycle jet/‘combined M3A2 Ramjet/scramjet/pulse M6A1 Composite structures, laminates, and manufactures thereof, specially designed for designed specially thereof, manufactures and laminates, structures, M6A1 Composite

or or

or or in 1C008 or 1C009.b.; 1C007; in specified a. Materials 1C010; in specified materials” filamentary or b. “Fibrous c. Aluminides specified in 1C002.a.; in specified c. Aluminides 1C002.a.; by specified c. Aluminides b. “Fibrous or filamentary materials” specified in 1C010; in specified materials” filamentary or b. “Fibrous actively the dynamic response or distortion of “spacecraft” structures; the dynamic of “spacecraft” response actively or distortion % of total rated kN/kg and a response time (the time required to achieve 90 ms. than 30 of less start-up) thrust from 3. in 1C007; specified “composite” materials “matrix” Ceramic Note: The weight cut-off is not relevant for nose cones. in 9A005 systems specified specified to 9A009 using manufactured any of the following: resins and 1C010.e. in specified materials” filamentary or 1. “Fibrous 2. by any “composites” reinforced of the following: Metal “matrix” 3. in 1C007; specified “composite” materials “matrix” Ceramic c. Structural components and isolation systems, specially designed to control 1 than more or to equal ratios thrust-to-weight with engines rocket liquid d. Pulsed b. Components and structures, specially designed for launch vehicle propulsion launch vehicle designed for specially b. Components and structures,

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Technical Note: 3.A.2., are the engines engines’ In Item that employ two ‘combined cycle or more turboprop, following of engines: gas-turbine engine of the (turbojet, types cycles turbofan and turboshaft), ramjet, scramjet, pulse jet, detonation engine, and rocket motor (liquid/solid-propellant hybrid). and components target drones and reconnaissance drones) capable of delivering at least a km. kg 300 “payload” of at least to a “range” 500 combustion, and specially designed components therefor, usable in the systems the in usable components therefor, designed specially combustion, and specified in 1.A. or 19.A.2. M19A ITEM 19 OTHER COMPLETE DELIVERY SYSTEMS: equipment, assemblies assemblies equipment, SYSTEMS: DELIVERY COMPLETE OTHER 19 M19A ITEM M1A2 Complete unmanned aerial vehicle systems (including cruise missile systems, missile cruise (including systems vehicle aerial unmanned M1A2 Complete M3A2 Ramjet/scramjet/pulse jet/‘combined cycle engines’, including devices to regulate to devices including engines’, cycle jet/‘combined M3A2 Ramjet/scramjet/pulse

and 1 hour; to or exceeding 46,3 km/h (25 knots); to or exceeding 46,3

a. A maximum ‘endurance’ greater than or equal to 30 minutes but less than less but minutes 30 to equal or than greater ‘endurance’ maximum a. A b. Designed to take-off and have stable controlled flight in wind gusts equal gusts wind in flight controlled stable have and take-off to b. Designed flight. unmanned “airship” or “UAV” commands the conditions (ISO 2533:1975) in zero wind. at sea level direct ‘natural vision’ of the ‘operator’ and having vision’ of the ‘operator’ ‘natural any direct of the following: following: the of all 1. Having Technical Notes: 1. For the purposes of 9A012.a., ‘operator’ is a person who initiates or For the purposes of 9A012.a., ‘endurance’ is to be calculated for ISA 2. 2. A maximum ‘endurance’ of 1 hour or greater; and components, as follows: and components, as 9A112. ALSO N.B.: SEE a. “UAVs” or unmanned designed “airships”, to have flight out of the controlled therefor. 9A118. AND 9A111 ALSO N.B.: SEE 9A012 “Unmanned aerial vehicles” (“UAVs”), unmanned “airships”, related equipment related “airships”, unmanned (“UAVs”), vehicles” aerial 9A012 “Unmanned 9A011 Ramjet, scramjet or combined cycle engines, and specially designed components designed specially and engines, cycle combined or scramjet 9A011 Ramjet,

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–1 h

–1

aircraft or in quantities appropriate for replacement parts for a manned aircraft. excluding civil certified engines with a ‘maximum thrust value’ greater value’ thrust ‘maximum a with engines certified excluding civil and than 8,89 un-installed); kN (achieved continuous power at sea level static conditions using the ICAO standard ICAO the using conditions static level sea at continuous power atmosphere); 1. ‘Maximum thrust value’ greater than N 400 (achieved un-installed) 2. Specific fuel consumption kg of N 0,15 Note: Engines specified in 3.A.1. may be exported as part of a manned Technical Note: In 3.A.1.a.1., ‘maximum thrust value’ is the manufacturer's demonstrated type certified maximum The civil thrust for the engine type un-installed. be equal thrust value will than to or less the manufacturer's demonstrated type. engine the for maximum thrust consumption. fuel or specific of thrust regardless a. Engines having both of the following characteristics: following the of both having a. Engines gyros specified in 9.A.4. or 9.A.5., and systems incorporating such equipment, 9.A.5., 9.A.4. incorporating in or and systems gyros specified designed components therefor. and specially b. Engines designed in 1.A. or modified for systems specified or 19.A.2., b. M3A1 Turbojet and turbofan engines, as follows: as engines, turbofan and M3A1 Turbojet M9A6 9.A.5. or 9.A.3. or in specified accelerometers using equipment other or Inertial

and

with or without corrective lenses. without corrective with or excluding civil certified engines with a ‘maximum thrust value’ greater value’ thrust ‘maximum a engines with certified excluding civil un-installed), N (achieved 890 than 8 power at sea level static conditions power using at sea level static the ICAO standard atmosphere); 1. ‘Maximum thrust value’ greater than N 400 (achieved un-installed) Technical Note: For the purpose of 9A101.a.1. ‘maximum the manufacturer's thrust value’ is type civil The un-installed. type engine the for demonstrated maximum thrust certified thrust value will be equal or less than the manufacturer's demonstrated type. engine the for maximum thrust specified in 9A012 or 9A112.a., 3. For the purposes of 9A012.a., ‘natural vision’ means unaided human sight, human unaided means vision’ ‘natural 9A012.a., of purposes the 3. For used 1. Not used 2. Not manned to a “UAV”unmanned in 9A012.a.; or “airship”, specified “airship”, designed or modified to propel “UAVs” or unmanned at altitudes “airships”, 000 feet). (50 metres 240 above 15 2. Specific fuel consumption of 0,15 kg/N/hr or less (at maximum continuous maximum (at less or kg/N/hr 0,15 of consumption fuel 2. Specific 3. Equipment or components, or designed specially to convert a manned “aircraft” a. Engines having both of the following characteristics: following the of both having a. Engines b. Engines designed or modified for use in “missiles” or unmanned aerial vehicles aerial unmanned or “missiles” in use for modified or designed b. Engines b. Related equipment and components, as follows: as components, and equipment b. Related specially engines, type combustion internal rotary or reciprocating breathing 4. Air 9A101 Turbojet and turbofan engines, other than those specified in 9A001, as follows; as 9A001, in specified those than other engines, turbofan and 9A101 Turbojet

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 243

Ns, but less than 1,1 × 10 than 1,1 Ns, but less

Ns; 5

6 designed or modified to be integrated, into a liquid propellant or gel propellant into a liquid propellant designed modified to be integrated, or than greater or to equal capacity impulse total a has which propulsion system 8,41 × 10 vehicles, and sounding rockets) capable of delivering at least a 500 kg vehicles, and a 500 sounding least capable of delivering at rockets) km. 300 “payload”of at least to a “range” 19.A.2., and specially designed components therefor, having a maximum power maximum a having therefor, components designed specially 19.A.2., and kW (achieved uninstalled at sea level static conditions using the greater than 10 engines. certified excluding civil atmosphere), ICAO standard Technical Note: of 3.A.9., incorporates all a ‘turboprop Item For the purposes engine system’ of the following: a. Turboshaftengine; and b. Power transmission system to transfer the power to a propeller. vehicles, and sounding in 1.A.1., not specified “range” rockets), capable of a km. than 300 equal to or greater designed or modified to be integrated, into a liquid propellant or gel propellant into a liquid propellant designed modified to be integrated, or than greater or to equal capacity impulse total a has which propulsion system 1,1 × 10 M3A9 ‘Turboprop engine systems’ specially designed for the systems in 1.A.2. or 1.A.2. in systems the for designed specially systems’ engine M3A9 ‘Turboprop launch space systems, missile ballistic (including systems rocket M1A1 Complete M19A1 Complete rocket systems (including ballistic missile systems, space launch space systems, missile ballistic (including systems rocket M19A1 Complete M2A1c2 Liquid propellant rocket engines or gel propellant rocket motors integrated, or M20A1b2 Liquid propellant rocket engines or gel propellant rocket motors integrated, or

and unmanned aerial vehicles, capable of a range of 300 km, other than those unmanned vehicles, capable of a range 300 aerial specified in 9A005 or 9A105.a., integrated, or designed or modified to be integrated, into a liquid propellant propulsion system which has a total than 0,841 MNs equal to or greater impulse capacity b. Power transmission to transfer the power system to a propeller. level static conditions using ICAO standard atmosphere. into a liquid in 9A005, designed to be integrated, or or modified integrated, equal to or propellant propulsion impulse capacity system which has a total greater than 1,1 MNs; following: engine; a. Turboshaft Note: 9A102 does not control civil certified engines. certified civil control not does Note: 9A102 b. Liquid propellant rocket engines, usable in complete rocket systems or specified in 9A012 or 9A112.a., and specially designed components therefor, kW. than having 10 power’ greater a ‘maximum 9A004. ALSO N.B.: SEE 9A119. ALSO N.B.: SEE specified those than other “missiles”, in usable engines rocket propellant a. Liquid Technical Notes: 1. For the purposes of 9A102 a ‘turboprop incorporates engine all of the system’ 2. For the purposes of 9A102 the ‘maximum power’ is achieved uninstalled at sea 9A105 Liquid propellant rocket engines, as follows: as engines, rocket propellant 9A105 Liquid 9A104 km. Sounding 300 rockets, capable of a range at least 9A102 ‘Turboprop engine systems’ specially designed for unmanned aerial vehicles aerial unmanned for designed specially systems’ engine 9A102 ‘Turboprop

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 244

following: systems specified in 1.A. systems specified or 19.A.1. Note: to 3.C.2. Refer for ‘insulation’ material in bulk or sheet form. Technical Note: control: vector thrust achieving of methods following the 2.A.1.e. includes nozzle; a. Flexible injection; gas secondary or b. Fluid nozzle; or engine c. Movable probes); or vanes (jet stream gas exhaust of d. Deflection tabs. thrust of e. Use in 1.A., designed components specially usable in the systems specified therefor, g rms designed than 10 or modified to operate in vibration environments greater Hz and 2 kHz. between 20 Notes: 3.A.5. pumps in are the valves, and 1. The only servo gas turbines specified Technical Note: In 3.A.3. intended to be applied components ‘insulation’ to the a rocket motor, of case closures, includes cured or semi-cured case, nozzle inlets, i.e. the compounded rubber components comprising sheet stock containing an insulating or refractory material. It may also be incorporated boots as stress relief or flaps. as provided in the Note below 2.A.1. for those designed for rocket systems that rocket Note below those designed for 2.A.1. as provided in the for 1.A.; in specified systems of capability “range”/“payload” the exceed do not Technical M3A3 Rocket motor cases, ‘insulation’ components and nozzles therefor, usable in the in usable therefor, nozzles and components ‘insulation’ cases, motor M3A3 Rocket M3A5 Liquid, slurry and gel propellant (including oxidisers) control systems, and systems, control oxidisers) (including propellant gel and slurry M3A5 Liquid, M2A1e Thrust vector control subsystems, in 1.A., usable in the systems specified except or

the following: specially designed components designed usable in “missiles”, therefor, or between g rms than 10 environments greater in vibration to operate modified 20 Hz and 2 kHz; launch vehicles specified in 9A004 or sounding rockets specified in 9A104; or sounding in 9A104;rockets specified Note: The only servo valves, pumps and gas turbines specified in 9A106.d., are 9A106.d., in specified turbines gas and pumps valves, servo only Note: The Technical Note: in 9A106.c. control specified Examples of methods achieving thrust vector of are: nozzle; 1. Flexible injection; gas secondary or 2. Fluid nozzle; or engine 3. Movable probes); or vanes (jet stream gas exhaust of 4. Deflection tabs. 5. Thrust d. Liquid, slurry and gel propellant (including oxidisers) control systems, and designed for liquid rocket propulsion systems: rocket liquid designed for space “missiles”, in usable chambers, combustion or thrust for liners a. Ablative 9A004 in specified vehicles launch space “missiles”, in usable nozzles, b. Rocket “missiles”; in usable sub-systems, control vector c. Thrust 9A106 in 9A006 Systems or components, than those specified other as follows, specially

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 245

Ns;

Ns, but less than 1,1 × 10 than 1,1 Ns, but less

minute, at an absolute pressure equal to or greater than 7 MPa, that have ms. than 100 less of response time an actuator 8 000 rpm at the maximum operating mode 7 MPa. than greater or equal to or with discharge pressures maximum operating mode. the 000 rpm at than 8 or greater a. Servo valves designed for flow rates equal to or greater than 24 litres per litres 24 than greater or to equal rates flow for designed valves a. Servo than greater or to equal speeds shaft with propellants, liquid for b. Pumps, c. Gas turbines, for liquid propellant turbopumps, with shaft speeds equal to satellite. capacity equal to or greater than 8,41 × 10 capacity equal to than or 8,41 greater In 3.A.3. intended to be applied components ‘insulation’ to the a rocket motor, of case closures, includes cured or semi-cured case, nozzle inlets, i.e. the compounded rubber components comprising sheet stock containing an insulating or refractory material. It may also be incorporated boots as stress relief or flaps. Note: to 3.C.2. Refer for ‘insulation’ material in bulk or sheet form. systems specified in 1.A. systems specified or 19.A.1. 2. Systems and components specified in 3.A.5. may be exported as part of a of part as exported be may 3.A.5. in specified components and 2. Systems the subsystems specified in 2.A.1.c.2. the subsystems specified or 20.A.1.b.2. Technical Note: Technical M3A3 Rocket motor cases, ‘insulation’ components and nozzles therefor, usable in the in usable therefor, nozzles and components ‘insulation’ cases, motor M3A3 Rocket M3A3 M3A10 Combustion chambers and nozzles for liquid propellant rocket engines usable in usable engines rocket propellant liquid for nozzles and chambers M3A10 Combustion M20A1b1 Solid rocket motors or hybrid motors having propellant rocket impulse a total

per minute, at an absolute pressure equal to or greater than 7 MPa, an absolute pressure equal to or greater per minute, at ms; that have an actuator of less than response 100 time discharge with a maximum operating mode or 000 r.p.m. at than 8 or greater than pressures equal to 7 MPa. 000 equal to or greater than r.p.m. 8 at the maximum operating mode. a. Servo valves designed for flow rates equal to or greater than 24 litres 24 than greater or to equal rates flow for designed valves a. Servo greater or to equal speeds shaft with propellants, liquid for b. Pumps, speeds shaft with turbopumps, propellant liquid for turbines, c. Gas space launch vehicles specified in 9A004 or sounding rockets specified in 9A104; or sounding in 9A104;rockets specified specified in 9A004 or sounding rockets specified in 9A104. aerial vehicles, capable of a range of 300 km, other than those specified in 9A007, km, other than those specified vehicles, capable of a range 300 aerial 0,841 MNs. than greater or to equal capacity impulse having total 9A119. ALSO N.B.: SEE a. Rocket motor cases and “insulation” components therefor, usable in “missiles”, “missiles”, in for solid rocket propulsion systems: usable therefor, components “insulation” and cases motor a. Rocket 9A004 in specified vehicles launch space “missiles”, in usable nozzles, b. Rocket e. Combustion chambers and nozzles, usable in “missiles”, space launch vehicles launch space “missiles”, in usable nozzles, and chambers e. Combustion 9A107 Solid propellant rocket engines, usable in complete rocket systems or unmanned or systems rocket complete in usable engines, rocket propellant 9A107 Solid 9A108 Components, other than those specified in 9A008, as follows, specially designed specially follows, as 9A008, in specified those than other 9A108 Components,

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Ns, but less than 1,1 × 10 than 1,1 Ns, but less

Ns; 5

6 Ns;

Ns, but less than 1,1 × 10 than 1,1 Ns, but less

5 capacity equal to or greater than 8,41 × 10 than 8,41 capacity equal to or greater designed into or modified to be a liquid propellant or gel integrated, than greater or to equal capacity impulse total a has which propulsion system 8,41 × 10 capacity equal to or greater than 1,1 × 10 capacity equal to than or greater 1,1 specified in 19.A.1., as follows: 1. Solid propellant rocket motors or hybrid rocket motors having a total impulse Technical Note: control: vector thrust achieving of methods following the 2.A.1.e. includes nozzle; a. Flexible injection; gas secondary or b. Fluid nozzle; or engine c. Movable probes); or vanes (jet stream gas exhaust of d. Deflection tabs. thrust of e. Use 2. Liquid propellant rocket engines gel propellant rocket motors integrated, or or 1. Solid propellant rocket motors or hybrid rocket motors having a total impulse and 20.A.1.b.1. as provided in the Note below 2.A.1. for those designed for rocket systems that rocket Note below those designed for 2.A.1. as provided in the for 1.A.; in specified systems of capability “range”/“payload” the exceed do not M3A6 Specially designed components for hybrid rocket motors specified in 2.A.1.c.1. in specified motors rocket hybrid for components designed M3A6 Specially M2A1c Rocket in 1.A., propulsion specified as follows; subsystems, usable in the systems M2A1e Thrust vector control subsystems, in 1.A., usable in the systems specified except M20A1b Rocket propulsion subsystems, in 2.A.1., not specified usable in the systems or

Technical Note: in 9A108.c. control specified methods vector of achieving thrust Examples of are: nozzle; 1. Flexible injection; gas secondary or 2. Fluid nozzle; or engine 3. Movable probes); or vanes (jet stream gas exhaust of 4. Deflection vehicles, capable of 300 km, in 9A009, other than those specified having total a vehicles, capable of 300 than 0,841 designed MNs, to or greater and specially equal impulse capacity components therefor; usable in “missiles”. that are 5. Thrust tabs. 5. Thrust a. Hybrid rocket motors usable in complete systems or unmanned aerial 9A009 in specified motors rocket hybrid designed components for b. Specially 9A119. and 9A009 ALSO N.B.: SEE c. Thrust vector control sub-systems, usable in “missiles”. in usable sub-systems, control vector c. Thrust 9A109 Hybrid rocket motors and specially designed components as follows: as components designed specially and motors rocket 9A109 Hybrid

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 247

Ns;

in 2.A.1.c.2., may designed be treated or modified for use on satellites, exported subject to end-use the subsystem is as Category if II, statements and quantity appropriate limits for the excepted end-use stated above, when having a vacuum thrust not greater than 1kN. designed or modified to be integrated, into a liquid propellant or gel or liquid propellant into a be integrated, designed to or modified propellant propulsion system which has impulse capacity equal to a total × 10 than 1,1 or greater Note: Liquid propellant apogee engines or station-keeping engines specified engines station-keeping or engines apogee propellant Note: Liquid 2. Liquid propellant rocket engines or gel propellant rocket motors integrated, or integrated, motors rocket propellant gel or engines rocket propellant 2. Liquid in 1.A., 19.A.1. use in the systems specified or 19.A.2. and the subsystems specified in 2.A. or 20.A. combustion, and specially designed components therefor, usable in the systems the in usable components therefor, designed specially combustion, and specified in 1.A. or 19.A.2. Technical Note: 3.A.2., are the engines engines’ In Item that employ two ‘combined cycle or more turboprop, following of engines: gas-turbine engine of the (turbojet, types cycles turbofan and turboshaft), ramjet, scramjet, pulse jet, detonation engine, and rocket motor (liquid/solid-propellant hybrid) M6A1 Composite structures, laminates, and manufactures thereof, specially designed for designed specially thereof, manufactures and laminates, structures, M6A1 Composite M3A2 Ramjet/scramjet/pulse jet/‘combined cycle engines’, including devices to regulate to devices including engines’, cycle jet/‘combined M3A2 Ramjet/scramjet/pulse

9A012 or 9A112.a., and specially designed components therefor. designed specially 9A112.a., and 9A012 or 9A118. AND 9A011 ALSO N.B.: SEE specified in 9A010, specified or the designed subsystems use specially for in ‘missiles’ 9A119. 9A005, 9A007, 9A106.c., 9A107, 9A108.c., 9A105,9A116 or in specified 1A002. ALSO N.B.: SEE Technical Note: and means systems unmanned In 9A110 complete rocket ‘missile’ aerial vehicle km. systems capable of a range exceeding 300 9A111 Pulse jet engines, usable in “missiles” or unmanned aerial vehicles specified in specified vehicles aerial unmanned or “missiles” in usable engines, jet 9A111 Pulse 9A110 Composite structures, laminates and manufactures thereof, other than those than other thereof, manufactures and laminates structures, 9A110 Composite

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recreational or competition purposes. human operator; and human operator; greater than 20 or litres; than 20 litres. greater mechanism with a capacity products or additives, as part of the “payload” to be dispersed in the atmos crop dusting and for dry pesticides aerosols include phere. Examples of chemicals for cloud seeding. 1. An autonomous flight control and navigation capability; or capability; navigation and control flight autonomous 1. An vision 2. range involving out of the direct a flight Capability of controlled 1. Incorporating an aerosol dispensing system/mechanism with a capacity 2. Designed or modified to incorporate an aerosol dispensing system/ and launching in 1.A., of the systems specified 19.A.1., or 19.A.2. launching of the systems specified in 1.A. in specified systems the launching of Technical Notes: by- components, fuel than other liquids or particulate of consists aerosol 1. An target drones and reconnaissance drones), not specified in 1.A.2., capable of a km. than 300 “range” equal to greater or having all of the following: the of having all following: the of any a. Having following: the of any b. Having Note: Item 19.A.3. does not control model aircraft, specially designed for M12A1 Apparatus and devices, designed or modified for the handling, control, activation control, handling, the for modified or designed devices, and M12A1 Apparatus M12A2 Vehicles designed or modified for the transport, handling, control, activation and activation control, handling, transport, the for modified or designed M12A2 Vehicles M19A2 Complete unmanned aerial vehicle systems (including cruise missile systems, missile cruise (including systems vehicle aerial unmanned M19A2 Complete M19A3 Complete unmanned aerial vehicle systems, not specified in 1.A.2. or 19.A.2., or 1.A.2. in specified not systems, vehicle aerial unmanned M19A3 Complete or

and greater than 20 litres; mechanism with a capacity greater than 20 litres. greater mechanism with a capacity human operator; a. Incorporating an aerosol dispensing system/mechanism with a capacity capacity a with system/mechanism dispensing aerosol an a. Incorporating a. An autonomous flight control and navigation capability; navigation and control flight autonomous a. An b. Designed or modified to incorporate an aerosol dispensing system/ products or additives, as part of the “payload” to be dispersed in the and dusting crop for pesticides include aerosols of atmosphere. Examples dry chemicals for cloud seeding. storage and for necessary which are hydraulic, etc.), anical, electrical, dispersion of an aerosol into the atmosphere. This includes the possibility the combustion into of aerosol exhaust vapour injection and into the stream. propeller slip b. Capability of controlled flight out of the direct vision range involving a involving range vision direct the of out flight controlled of b. Capability or modified for space launch vehicles specified in 9A004, specified space launch vehicles sounding or modified for rockets in 9A104 specified in 9A012 or unmanned vehicles specified aerial or 9A112.a.; modified for space launch vehicles specified in 9A004 specified space launch vehicles or sounding modified for rockets specified in 9A104. 2. Having any of the following: the of any 2. Having 1. Having any of the following: the of any 1. Having 1. An aerosol consists of particulate or liquids other than fuel components, by components, Technical Notes: fuel than other liquids or particulate of consists aerosol 1. An (mech devices those all contains system/mechanism dispensing aerosol 2. An a. Apparatus and devices for handling, control, activation or launching, designed launching, or activation control, handling, for devices and a. Apparatus b. Vehicles for transport, handling, control, activation or launching, designed or designed launching, or activation control, handling, transport, for b. Vehicles follows: a. km; capable of a range 300 (“UAVs”) “Unmanned vehicles” aerial following: the of all having (“UAVs”) vehicles” aerial b. “Unmanned 9A115 Launch support equipment as follows: as equipment support 9A115 Launch 9A112 “Unmanned aerial vehicles” (“UAVs”), other than those specified in 9A012, as 9A012, in specified those than other (“UAVs”), vehicles” aerial 9A112 “Unmanned

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materials; capacity materials; Pyrotechnic bolts, nuts and shackles; and nuts bolts, Pyrotechnic locks; Ball devices; cutting Circular (FLSC). charges shaped linear Flexible the systems specified in 1.A. the systems specified combustion, and specially designed components therefor, usable in the systems the in usable components therefor, designed specially combustion, and specified in 1.A. or 19.A.2. systems specified in 1.A., systems specified as follows, except provided in the Note below 2.A.1. for those designed for non-weapon payloads: 1. Heat shields, and components therefor, fabricated of ceramic or ablative 2. Heat sinks and components therefor, fabricated of light-weight, high heat vehicles; re-entry for designed specially equipment 3. Electronic Technical Note: 3.A.2., are the engines engines’ In Item that employ two ‘combined cycle or more turboprop, following of engines: gas-turbine engine of the (turbojet, types cycles turbofan and turboshaft), ramjet, scramjet, pulse jet, detonation engine, and rocket motor (liquid/solid-propellant hybrid). Note: See also Item 11.A.5. Item also Note: See Technical Note: the of contain some 3.A.4. may in specified Staging and separation mechanisms following components: — — — — M3A4 Staging mechanisms, separation mechanisms, and interstages therefor, usable in usable therefor, interstages and mechanisms, separation mechanisms, M3A4 Staging M3A2 Ramjet/scramjet/pulse jet/‘combined cycle engines’, including devices to regulate to devices including engines’, cycle jet/‘combined M3A2 Ramjet/scramjet/pulse M2A1b usable in the vehicles, and equipment designed Re-entry therefor, or modified

materials; capacity materials; N.B.: SEE ALSO 9A121. ALSO N.B.: SEE or unmanned aerial vehicles specified in 9A012 or 9A112.a., specified in 9A011 or in 9A112.a., specified 9A012 or in specified vehicles unmanned aerial or 9A111. therefor, as follows: vehicles; a. Reentry or ablative of ceramic Heat shields and components fabricated therefor, b. c. Heat sinks and components therefor, fabricated of light-weight, high heat vehicles. reentry for designed specially equipment d. Electronic 9A117 usable in “missiles”. mechanisms, and interstages, Staging mechanisms, separation 9A118 combustion usable in engines, usable in “missiles” Devices to regulate which are 9A116 Reentry vehicles, usable in “missiles”, and equipment designed or modified or designed equipment and “missiles”, in usable vehicles, 9A116 Reentry

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with dimension of the ‘test cross section size’ equal to or less than section size’ with dimension cross of the ‘test 250 mm. study of airflow over objects. systems specified in 1.A. in 2.A. or 19.A. subsystems or 20.A. systems specified or the specified Note: 15.B.2 Item does speeds not control wind of Mach 3 or less tunnels for 4.C. in 1.A.1. used in the systems specified or other liquid propellants specified in 1.A.1. or 19.A.1. Technical Note: to Interstage connectors in 11.A.5. connectors referred also include electrical installed between systems specified in 1.A.1. or 19.A.1. and their “payload”. Technical Notes: 1. includes wind tunnels and shock tunnels for the facilities’ ‘Aerodynamic test 2.A.1., in 19.A. usable in systems specified Missile Technology Control Regime (M.TCR): Equipment, software and technology annex M3A8 Liquid propellant tanks specially designed for the propellants controlled in Item in controlled propellants the for designed specially tanks propellant M3A8 Liquid M2A1a in 1.A.; specified stages usable in the systems Individual rocket M15B2 for speeds of Mach 0,9 the or more, usable for facilities’ ‘Aerodynamic test M11A5 Umbilical and interstage electrical connectors specially designed for systems for designed specially connectors electrical interstage and M11A5 Umbilical M20A1a in stages, not specified a. Individual rocket Complete subsystems as follows:

of dual-use items

educational purposes and having a ‘test section size’ (measured size’ section educational purposes and ‘test having a mm. laterally) of less than 250 Note: 9B005.a. does not control wind tunnels specially designed for propellants specified in 1C111 systems used liquid propellants’, propellants specified in rocket or ‘other km. kg payload 300 least to a range of at a 500 at least capable of delivering space launch vehicles specified in 9A004 or sounding rockets specified in 9A104. vehicles, capable of a range of 300 km, other than those specified in 9A005, vehicles, capable of a range of 300 9A109.and 9A107 9A007, 9A009, 9A105, Technical Note: connectors to in 9A121 connectors referred also include electrical Interstage installed between the space “missile”, launch or vehicle sounding rocket and their payload. automated data acquisition and processing equipment, specially designed automated data acquisition and processing equipment, use specially for with any following: of the 9B105. ALSO N.B.: SEE a. more; 1,2 or Mach of speeds designed for Wind tunnels 9B005 On-line (real time) control systems, instrumentation (including sensors) or sensors) (including instrumentation systems, control time) (real 9B005 On-line 9A120 Liquid propellant tanks, other than those specified in 9A006, specially designed for designed specially 9A006, in specified those than other tanks, propellant 9A120 Liquid 9A121 Umbilical and interstage electrical connectors specially designed for “missiles”, “missiles”, for designed specially connectors electrical interstage and 9A121 Umbilical 9A119 Individual rocket stages, usable in complete rocket systems or unmanned aerial unmanned or systems rocket complete in usable stages, rocket 9A119 Individual The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/ Council Regulation (EC) in identified corresponding equipment and components as systems, The 2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit and brokering transfer, exports, of control the for Community regime a 5 up setting 2009 of 2009 May Equipment Production and Inspection 9B Test, M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 251

) or with a total rated acoustic power output rated ) or with a total of

2 N/m

–5

with dimension of the ‘test cross section size’ equal to or less than equal to or less size’ cross section the ‘test with dimension of 250 mm. (referenced to 2 × 10 (referenced to 2 4 kW or greater; and °C. °C to above 125 Temperature range from below –50 square, at or longest side of the rectangle, or major axis of the ellipse the the section is cross section’ location. ‘Test cross section’ ‘test the largest direction. flow the perpendicular to study of airflow over objects. square, or the longest side of the rectangle, or the major axis of at the ellipse the cross largest section’ location. cross ‘test is ‘Test section’ the section direction. flow the perpendicular to systems specified in 1.A. in 2.A. or 19.A. subsystems or 20.A. systems specified or the specified conditions: 1. dB or greater sound Acoustic environments at an overall of 140 level pressure 2. Any of the following: a. Altitude equal to or greater than 15 km; or b. than 15 Any equal to or greater of the following: a. Altitude 2. 2. of the or the side means the diameter of circle, size’ cross section ‘Test Note: 15.B.2 Item does not control wind tunnels for speeds of Mach 3 or less Technical Notes: 1. includes wind tunnels and shock tunnels for the facilities’ ‘Aerodynamic test 2. or the side of means the diameter of circle, cross section size’ ‘Test M15B2 for speeds of Mach 0,9 the or more, usable for facilities’ ‘Aerodynamic test M15B4b of the following flight all Environmental chambers capable of simulating

Pa) with a rated output of 4 kW or more at a kW at or more output of 4 with a rated Pa) μ

dimension of the ‘test cross section size’ equal to or less than 250 mm. than equal to or less 250 size’ cross section dimension ‘test of the hot-shot tunnels, plasma arc tunnels, shock and tunnels tubes, shock tunnels, gas arc hot-shot tunnels, plasma light gas guns; simulating Reynolds number flows exceeding 25 × 10 simulating Reynolds number flows exceeding 25 for the study of airflow over objects. major of or the axis square, the rectangle, the of of or the longest side the side is the cross section’ location. ‘Test cross section’ ‘test at the largest the ellipse section perpendicular to the flow direction. Technical Note: means or the ‘Test section size’ diameter of the circle, the side of the square, or location. section test the longest side of rectangle, at largest b. Devices for simulating flow-environments at speeds exceeding Mach 5, including 5, Mach exceeding speeds at flow-environments simulating for b. Devices c. Wind c. Wind tunnels or devices, other than two-dimensional sections, capable of 160 dB or more (referenced to 20 °C), and specially designed quartz 000 273 K (1 exceeding test cell temperature 1 heaters therefor. 9B106. ALSO N.B.: SEE Technical Notes: tunnels shock and tunnels wind includes facilities’ test ‘aerodynamic 9B105 1. In 2. or means diameter of the circle, size’ the In Note to 9B105, cross section ‘test Note: 9B105 does not control wind-tunnels Note: for speeds of Mach 3 or less with and their subsystems. and their 9B005. ALSO N.B.: SEE 9B006 Acoustic vibration test equipment capable of producing sound pressure levels of levels pressure sound producing of capable equipment test vibration 9B006 Acoustic 9B105 ‘missiles’ speeds of Mach 0,9 usable for for or more, facilities’ ‘Aerodynamic test

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 252

) or with a total rated acoustic

N/m

–5

vibration environment with a single wave (e.g. a sine wave) and wave) a sine wave (e.g. a single vibration environment with systems capable of generating a broad band random vibration (i.e. power spectrum). incor to devices) sealing (e.g. interfaces appropriatechamber provides porate a in equipment shaker unit or as specified other vibration test this Item. a. Altitude equal to or greater than 15 km; or km; 15 than greater or to equal a. Altitude and °C; 125 above to °C –50 below from range b. Temperature equipment to produce environments to vibration test vibration equal or greater than 10 g rms, measured ‘bare than 5 kN; equal to or greater forces while imparting table’, between 20 Hz and 2 kHz greater (referenced to 2 × 10 to greater (referenced 2 Technical Notes: 1. Item 15.B.4.a.2. describes systems that are capable of generating a 2. In Item 15.B.4.a.2., designed or modified means the environmental and kW or greater; power output of 4 1. Capable any of simulating of the following flight conditions: 2. Incorporating, or designed a or modified to shaker unit or other incorporate, conditions: dB or 1. Acoustic environments at an overall sound pressure level of 140 19.A. or the subsystems specified in 2.A. or 20.A.: 2.A. or in specified subsystems the 19.A. or characteristics: following the of all having chambers a. Environmental b. Environmental chambers capable of simulating all of the following flight all Environmental chambers capable of simulating b. M15B4 Environmental chambers as follows, usable for the systems specified in 1.A. or 1.A. in specified systems the for usable follows, as chambers M15B4 Environmental

and

(+125 °C); environment with a single wave (e.g., a sine wave) and systems capable and systems wave) a sine wave (e.g., a single environment with of generating a broad band random power vibration (i.e., spectrum). incorporate a to sealing devices) (e.g., provides appropriate interfaces in 2B116. equipment as specified shaker unit or other vibration test or fittings. other vibration test equipment to produce other vibration test vibration environments equal to or greater than 10 g rms, measured ‘bare table’, than 5 kN; equal to or greater forces while imparting between 20 Hz and 2 kHz b. Temperature range from below 223 K (–50 ° C) to above 398 K above to C) ° (–50 223 K below from range Temperature b. Technical Notes: vibration a generating of capable are that systems describes 1. 9B106.a.2. chamber environmental the means modified’ or ‘designed 9B106.a.2., 2. In fixture no with surface, or table, flat a means table’ ‘bare 9B106.a.2. 3. In a. Altitude equal to or greater than 15 km; 15 than greater or to equal a. Altitude 2. Incorporating, or ‘designed or modified’ to incorporate, a shaker unit 2. systems capable of a range exceeding 300 km. systems capable of a range exceeding 300 conditions: following: the of any 1. Having b. conditions: simulating the following flight capable of Environmental chambers 3. In 9B105 ‘missile’ means complete rocket systems and unmanned aerial vehicle aerial unmanned and systems rocket complete means ‘missile’ 9B105 3. In the following flight Environmental chambers capable of simulating all a. 9B106 Environmental chambers and anechoic chambers, as follows: as chambers, anechoic and chambers 9B106 Environmental

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a. Altitude equal to or greater than 15 km; or km; 15 than greater or to equal a. Altitude °C 125 above to °C –50 below from range b. Temperature 2. Any of the following: the of 2. Any in 3.A.1., 3.A.2., 3.A.3., 3.A.4., 3.A.5., 3.A.6., 3.A.8., 3.A.9., 3.A.10. or 3.C. 3.A.1., 3.A.2., 3.A.3., 3.A.4., 3.A.5., 3.A.6., 3.A.8., 3.A.9., 3.A.10. in or 3.C. 3.A.1., 3.A.2., 3.A.3., 3.A.4., 3.A.5., 3.A.6., 3.A.8., 3.A.9., 3.A.10. or 19.A.2. M2B2 “Production equipment” specially designed for the subsystems specified in 2.A. in specified subsystems the for designed specially equipment” M2B2 “Production 1.A in specified systems the for designed specially facilities” M1B1 “Production M2B1 “Production facilities” specially designed for the subsystems specified in 2.A. in specified subsystems the for designed specially facilities” M2B1 “Production M3B2 “Production equipment” specially designed for equipment or materials specified materials or equipment for designed specially equipment” M3B2 “Production in specified materials or equipment for designed specially facilities” M3B1 “Production M20B1 “Production facilities” specially designed for the subsystems specified in 20.A. in specified subsystems the for designed specially facilities” M20B1 “Production M20B2 “Production equipment” specially designed for the subsystems specified in 20.A. in specified subsystems the for designed specially equipment” M20B2 “Production M19B1 “Production facilities” specially designed for the systems specified in 19.A.1 or 19.A.1 in specified systems the for designed specially facilities” M19B1 “Production

or Pa) or with a total rated acoustic power output of 4 kW or power Pa) or with a total rated acoustic output of 4 μ and greater; (referenced to 20 3. Temperature range from below 223 K (–50 °C) to above 398 K (+125 °C). °C) to above 398 K (+125 below 223 from K (–50 range 3. Temperature 2. Altitude equal to or greater than 15 km; 15 than greater or to equal 2. Altitude in 9A005 components to 9A009,specified 9A011, 9A101, 9A102, 9A105 to 9A120. to 9A109, 9A111, 9A116 Technical Note: and means systems unmanned In 9B116 complete rocket ‘missile’ aerial vehicle km. systems capable of a range exceeding 300 9A004, or systems, sub-systems, and components specified in 9A005 to 9A009, to 9A005 in specified components and sub-systems, systems, 9A004, or ‘missiles’. or 9A120 to 9A109, 9A111, 9A116 9A011, 9A101, 9A102, 9A104 to 1. dB or greater Acoustic environments at an sound overall pressure level of 140 9B115 Specially designed “production equipment” for the systems, sub-systems and sub-systems systems, the for equipment” “production designed 9B115 Specially 9B116 Specially designed “production facilities” for the space launch vehicles specified in specified vehicles launch space the for facilities” “production designed 9B116 Specially

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or the subsystems specified in 2.A. or the subsystems or 20.A., specified which to handle have the capacity solid or liquid rockets, motors or engines propellant having than a thrust greater 68 kN, or which are capable of simultaneously axial thrust measuring the three components. 2.A.1.c.1. or specially designed for subsystems specified in 20.A.1.b.1. in specified subsystems for designed specially 2.A.1.c.1. or specified in 2.A.1.c.1. or specially designed for subsystems in specified 20.A.1.b.1. Technical Note: In 3.C.1. ‘interior lining’ suited for the bond between interface the solid polymer based liquid usually a is liner or insulating propellant and case the HTPB or other e.g. carbon or insulating materials filled dispersion of refractory polymer with added interior. a case be sprayed or screeded over curing agents to Technical Note: In 3.C.2. intended ‘insulation’ to be applied to the components of a rocket motor, case closures, includes cured or semi-cured case, nozzle inlets, i.e. the compounded rubber sheet stock containing an insulating or material. refractory It may also be incorporated as stress relief boots or flaps specified in 3.A.3. Missile Technology Control Regime (M.TCR): Equipment, software and technology annex M3C1 ‘Interior lining’ usable for rocket motor cases in the subsystems specified in specified subsystems the in cases motor rocket for usable lining’ M3C1 ‘Interior M3C2 motor cases in the subsystems rocket in bulk usable for form material ‘Insulation’ M15B3 in 1.A., specified the systems 19.A.1. Test benches/stands, usable for or 19.A.2. or

of dual-use items

b. Capable of simultaneously measuring the three axial thrust components. thrust axial three the measuring simultaneously of b. Capable Technical Note: and In 9C108 systems means rocket unmanned complete ‘missile’ aerial vehicle km. systems capable of a range exceeding 300 having either of the following characteristics: following the of having either a. than 68 thrust; kN of handle more to The capacity in 9A008, for rocket motor cases usable in “missiles” or specially designed for specially or “missiles” usable in cases motor in 9A008, rocket for ‘missiles’. 9B117 motors, Test benches rockets or rocket and stands for solid or liquid propellant test 9C108 “Insulation” material in bulk form and “interior lining”, other than those specified those than other lining”, “interior and form bulk in material 9C108 “Insulation” The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/ Council Regulation (EC) in identified corresponding equipment and components as systems, The 2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit and brokering transfer, exports, of control the for Community regime a 5 up setting 2009 of 2009 May 9C Materials M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 255

divided by

2 m.

, measured at a temperature of (296 ± , measured at a temperature of (296

, measured at a temperature of (296 ± 2)K ((23 ± ± 2)K ((23 , measured at a temperature of (296

m and a specific modulus greater than 3,18 × 10 modulus than 3,18 m and a specific greater

4 using resins with a glass transition temperature (Tg), after cure, exceeding cure, after (Tg), a glass transition temperature with using resins °C as determined by ASTM D4065 or national equivalents. 145 2)°C) and a relative humidity of (50 ± 5)% 2)°C) and humidity of (50 a relative 2)K ((23 ± 2)°C) and a relative humidity of (50 ± 5)%. ± 2)°C) and humidity a of (50 relative 2)K ((23 the specific weight in N/m the specific divided by the specific weight divided by in N/m the specific designed or modified for “use” in the systems specified in 19.A.1.19.A.2. in or specified systems the in “use” for modified designed or specified in 3.A.2., 3.A.3. or 3.A.4. 2.A.1.c. in engines specified 2. In Item 6.C.1. ‘specific modulus’ is the Young's modulus in N/m in modulus Young's the is modulus’ ‘specific 6.C.1. Item 2. In specified in 6.A.1., made either with organic matrix or metal matrix utilising strength greater tensile having a specific reinforcements fibrous or filamentary × 10 than 7,62 Note: The only resin impregnated fibre prepregs specified in 6.C.1. are those 6.C.1. are in specified prepregs fibre impregnated resin only Note: The Technical Notes: 1. In Item 6.C.1. ‘specific tensile strength’ is the ultimate tensile strength in N/m Missile Technology Control Regime (M.TCR): Equipment, software and technology annex M6C1 Resin impregnated fibre prepregs and metal coated fibre preforms, for the goods M3D3 designed specially or modified for the “development” “Software” of equipment M2D2 motors or of rocket the “use” designed modified for specially or “Software” M19D1 “Software” which coordinates the function of more than one subsystem, specially subsystem, one than more of function the coordinates which M19D1 “Software”

4 ), after cure, ), after

of dual-use items those using resins with a glass transition temperature (T exceeding 418 K (145 °C) as determined by ASTM D4065 or equivalent. exceeding 418 K (145 required for detailed engine flow modelling; detailed required for

a. 2D or 3D viscous “software”, validated with wind tunnel or flight test data test flight a. wind tunnel or with validated 3D viscous “software”, 2D or “technology”,in 9A001 specified to 9A119, 9B or 9E003. in 9A001 specified to 9A119 or 9B. Note: The only resin impregnated fibre prepregs specified in entry 9C110 are composite structures, laminates and manufactures specified in 9A110, in made specified manufactures and laminates composite structures, either with organic matrix or metal matrix utilising fibrous or filamentary × 10 reinforcements having a “specific tensile strength” than greater 7,62 10 × 3,18 than greater modulus” “specific and a 1C210. AND 1C010 ALSO N.B.: SEE 9C110 Resin impregnated fibre prepregs and metal coated fibre preforms therefor, for 9D004 Other “software” as follows: as “software” 9D004 Other 9D001 “Software” specially designed or modified for the “development” of equipment or equipment of “development” the for modified or designed specially 9D001 “Software” 9D002 specially designed “Software” or modified for the “production” of equipment The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/ Council Regulation (EC) in identified corresponding equipment and components as systems, The 2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit and brokering transfer, exports, of control the for Community regime a 5 up setting 2009 of 2009 May 9D Software M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 256

specified in 1.B. 12.A.1. and flow-forming machines specified in 3.B.1. or 3.B.3. 3.B.1. or in specified machines and flow-forming specified in 2.B.1. or 19.A.2. 19.A.1. or 1.A., in specified systems testing for 15.B. usable 20.A. 2.A. or in subsystems specified M1D1 designed specially or modified for the “use” of “production “Software” facilities” M2D1 designed specially or modified for the “use” of “production “Software” facilities” M3D1 designed specially or modified for the “use” of “production “Software” facilities” M12D1 designed in specially “use” of equipment or modified for the specified “Software” M15D1 designed in specially “use” of equipment or modified for the specified “Software” and conditions in aero gas turbine engines; turbine gas aero conditions in combustion conditions, which have been validated with actual aero gas aero combustion with actual conditions, have been validated which data. or production) performance turbine engine (experimental specially designed to collect, reduce and time and analyse data in real articles feedback control, including dynamic of test adjustment capable of the is in progress; conditions, or test as the test growth in 9B001.a. in equipment specified 9B001.c.; material or crystal in 9A012; gas turbine blades, vans and “tip shrouds”; 1. and Specially designed aeromechanical combustion to aero thermal, predict 2. Theoretical modelling predictions of the aero thermal, aeromechanical and aeromechanical thermal, aero the of predictions modelling 2. Theoretical 9B105, 9B106, 9B116 or 9B117. or 9B105, 9B106, 9B116 b. “Software” b. “Software” for testing aero gas turbine engines, assemblies or components, single- or solidification designed to control directional specially c. “Software” used; d. Not e. specified operation of items designed the specially or modified for “Software” aero of passages cooling internal the design to designed specially f. “Software” following: the of all having g. “Software” 9D101 “Software” specially designed or modified for the “use” of goods specified in specified goods of “use” the for modified or designed specially 9D101 “Software”

M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 257

in 3.A.1. may be exported as part of a manned or as replacement aircraft “software” therefor. or as a satellite 3.A.5. of in exported as part may be specified systems replacement “software” therefor. the systems specified in 1.A. in 2.A or the subsystems the systems specified or 20.A. specified Notes: specified engines of “use” the for modified or designed specially 1. “Software” control propellant of “use” the for modified or designed specially 2. “Software” “Software” specially designed or modified for the “use” of rocket motors or of rocket the “use” designed modified for specially or “Software” 2.A.1.c. in engines specified maintenance of the operation or designed or modified for specially “Software” 2.A.1.b.3. in equipment specified subsystems or designed in specially “use” of equipment or modified for the specified “Software” 3.A.9. 3.A.1., 3.A.2., 3.A.4., 3.A.5., 3.A.6. or Technical Note: The modelling includes in particular the aerodynamic and thermodynamic analysis of the systems. M16D1 “Software” specially designed for modelling, simulation, or design integration of integration design or simulation, modelling, for designed specially M16D1 “Software” M20D1 “Software” specially designed or modified for the systems specified in 20.B.1. in specified systems the for modified or designed specially M20D1 “Software” M2D2 M2D4 M3D2 M2D5 M20D2

specially designed hardware specified in 4A102. the space launch vehicles specified in 9A004, in specified in 9A104 sounding launch the space vehicles specified rockets 9A005, in the subsystemsspecified 9A007, or 9A105, “missiles”, or 9A106.c., 9A119. or 9A107, 9A108.c., 9A116 Note: “Software” specified in 9D103 remains controlled when combined with 9A001, 9A005, 9A006.d., 9A006.g., 9A007.a., 9A008.d., 9A009.a., 9A010.d., 9A001, 9A005, 9A011, 9A101, 9A102, 9A105, 9A106.c., 9A106.d., 9A107, 9A108.c., 9A109, 9A118. or 9A111, 9A115.a., 9A116.d.,9A117 9D103 “Software” specially designed for modelling, simulation or design integration of integration design or simulation modelling, for designed specially 9D103 “Software” 9D104 “Software” specially designed or modified for the “use” of goods specified in specified goods of “use” the for modified or designed specially 9D104 “Software”

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duction” or “use” of a product. The may information of take the “technical form assistance”. data” or “technical duction” or “use” of a product. The may information of take the “technical form assistance”. data” or “technical one in 1.A. subsystem specified in systems designed or modified for “use” in the systems specified in 19.A.1.19.A.2. in or specified systems the in “use” for modified designed or “Software” specially designed “Software” or modified for the operation maintenance of 2.A.1.e. subsystems in in 2.D.2., not the “use” specified designed “Software”, specially or modified for in 20.A.1.b. of rocket motors or engines specified duction” or “use” of a product. The may information of take the “technical form assistance”. data” or “technical Missile Technology Control Regime (M.TCR): Equipment, software and technology annex M Means information which specific is required for the “development”, “pro M Means information which specific is required for the “development”, “pro M Means information which specific is required for the “development”, “pro M1D2 “Software” specially designed or modified to coordinate the function of more than more of function the coordinate to modified or designed specially M1D2 “Software” M19D1 “Software” which coordinates the function of more than one subsystem, specially subsystem, one than more of function the coordinates which M19D1 “Software”

of dual-use items

of goods in 9A101, specified 9A102, 9A104 to 9A111, 9A112.a. or 9A115 to 9A121. in 9A012 of ‘UAV’s specified or goods in 9A101, specified 9A102, 9A104 to 9A121. to 9A115 9A111, 9A112.a. or equipment materials, see 1E002.f. see equipment materials, equipment that specified in 9D003.e., that specified designed “use” in space launch specially for or modified vehicles specified in 9A004 or sounding rockets specified in 9A104 or ‘missiles’. Technical Note: and means systems complete rocket In 9D105 unmanned aerial vehicle ‘missile’ km. systems capable of a range exceeding 300 b. “Technology” according to the General Technology Note for the “production” 9E002 “Technology”“production”Technology the according to the General of Note for 9E101 a. “Technology” according to the General Technology Note for the “development” 9E001 “Technology” according to the General Technology Note for the “development” of “development” the for Note Technology General the to according 9E001 “Technology” 9D105 “Software” which coordinates the function of more than one subsystem, other than other subsystem, one than more of function the coordinates which 9D105 “Software” The corresponding systems, equipment and components as identified in Council Regulation (EC) No 428/ Council Regulation (EC) in identified corresponding equipment and components as systems, The 2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit and brokering transfer, exports, of control the for Community regime a 5 up setting 2009 of 2009 May 9E Technology M30 ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 259

______

Technical Note: In 9E101.b. means unmanned capable a range systems ‘UAV’ of aerial vehicle km. exceeding 300 launch in9A004, vehicles specified goods in 9A005 specified to 9A011, ‘UAV’s in 9A012 goods specified in 9A101,or specified 9A102, 9A104 to 9A111, 9A121, 9B105, 9B106, 9B115, 9B116, 9B117, 9D101 or 9A112.a., 9A115 to 9D103. Technical Note: means In 9E102 unmannedcapable of a range systems ‘UAV’ aerial vehicle km. exceeding 300 9E102 “Technology”Technology General according the “use” of space to the Note for

M30 M24 ▼ ▼ 02012R0267 — EN — 18.01.2017 — 022.003 — 260

▼M24 ANNEX VIIA

Software referred to in Article 10d 1. Enterprise Resource Planning software, designed specifically for use in nuclear and military industries Explanatory note: Enterprise Resource Planning software is software used for financial accounting, management accounting, human resources, manufacturing, supply chain management, project management, customer relationship management, data services, or access control.

02012R0267 — EN — 18.01.2017 — 022.003 — 261

▼M30 ANNEX VIIB

Graphite and raw, fabricated semi-finished metals referred to in Article 15a

HS Codes and descriptions

1. Raw or semi-fabricated graphite

2504 Natural graphite

3801 Artificial graphite; colloidal or semi-colloidal graphite; preparations based on graphite or other carbon in the form of pastes, blocks, plates or other semi- manufactures

2. Corrosion-resistant high-grade steel (Chromium-content > 12 %) in form of sheet, plate, tube or bar

ex 72 19 Flat-rolled products of stainless steel, of a width of 600 mm or more

ex 72 20 Flat-rolled products of stainless steel, of a width of less than 600 mm

ex 72 21 Bars and rods, hot-rolled, in irregularly wound coils, of stainless steel

ex 72 22 Other bars and rods of stainless steel; angles, shapes and sections of stainless steel

ex 72 25 Flat-rolled products of other alloy steel, of a width of 600 mm or more

ex 72 26 Flat-rolled products of other alloy steel, of a width of less than 600 mm

ex 72 27 Bars and rods, hot-rolled, in irregularly wound coils, of other alloy steel

ex 72 28 Other bars and rods of other alloy steel; angles, shapes and sections, of other alloy steel; hollow drill bars and rods, of alloy or non-alloy steel

ex 73 04 Tubes, pipes and hollow profiles, seamless, of iron (other than cast iron) or steel

ex 73 05 Other tubes and pipes (for example, welded, riveted or similarly closed), having circular cross-sections, the external diameter of which exceeds 406,4 mm, of iron or steel

ex 73 06 Other tubes, pipes and hollow profiles (for example, open seam or welded, riveted or similarly closed), of iron or steel

ex 73 07 Tube or pipe fittings (for example, couplings, elbows, sleeves), of iron or steel

3. Aluminium and alloys in form of sheet, plate, tube or bar

ex 76 04 Aluminium bars, rods and profiles

ex 7604 10 10 – Of aluminium, not alloyed

– – Bars and rods

ex 7604 29 10 – Of aluminium alloys 02012R0267 — EN — 18.01.2017 — 022.003 — 262

▼M30

– – Hollow profiles

– – – Bars and rods

7606 Aluminium plates, sheets and strip, of a thickness exceeding 0,2 mm

7608 Aluminium tubes and pipes

7609 Aluminium tube or pipe fittings (for example, couplings, elbows, sleeves)

4. Titanium and alloys in form of sheet, plate, tube or bar

ex 8108 90 Titanium and articles thereof, including waste and scrap

– Other

5. Nickel and alloys in form of sheet, plate, tube or bar

ex 75 05 Nickel bars, rods, profiles and wire

ex 7505 11 Bar and Rods

ex 7505 12

7506 Nickel plates, sheets, strip and foil

ex 75 07 Nickel tubes, pipes and tube or pipe fittings (for example, couplings, elbows, sleeves)

7507 11 – Tubes and pipes

– – Of nickel, not alloyed

7507 12 – Tubes and pipes

– – Of nickel alloys

7507 20 – Tube or pipe fittings

Explanatory note: the metal alloys in points 2, 3, 4 and 5 are those containing a higher percentage by weight of the stated metal than of any other element. 02012R0267 — EN — 18.01.2017 — 022.003 — 263

▼B ANNEX VIII

List of persons and entities referred to in Article 23(1) A. Persons and entities involved in nuclear or ballistic missiles activities

Natural persons

(1) Fereidoun Abbasi-Davani. Other information: Senior Ministry of Defence and Armed Forces Logistics (MODAFL) scientist with links to the Institute of Applied Physics. Working closely with Mohsen Fakhrizadeh-Mahabadi.

Date of UN designation: 24.3.2007.

▼M25 ______

▼B (3) Ali Akbar Ahmadian. Title: Vice Admiral. Function: Chief of Iranian Revolutionary Guard Corps (IRGC) Joint Staff.

Date of UN designation: 24.3.2007.

▼M25 ______

▼B (8) Bahmanyar Morteza Bahmanyar. Function: Head of Finance & Budget Dept, Aerospace Industries Organisation (AIO). Other information: Person involved in Iran's ballistic missile programme.

Date of UN designation: 23.12.2006.

▼M25 ______

▼B (11) Ahmad Vahid Dastjerdi. Function: Head of the Aerospace Industries Organisation (AIO). Other information: Person involved in Iran's ballistic missile programme.

Date of UN designation: 23.12.2006.

(12) Ahmad Derakhshandeh. Function: Chairman and Managing Director of Bank Sepah.

Date of UN designation: 24.3.2007.

(13) Mohammad Eslami. Title: Dr. Other information: Head of Defence Industries Training and Research Institute.

Date of UN designation: 3.3.2008.

(14) Reza-Gholi Esmaeli. Function: Head of Trade & International Affairs Dept, Aerospace Industries Organisation (AIO). Other information: Person involved in Iran's ballistic missile programme.

Date of UN designation: 23.12.2006.

(15) Mohsen Fakhrizadeh-Mahabadi. Other information: Senior MODAFL scientist and former head of the Physics Research Centre (PHRC).

Date of UN designation: 24.3.2007.

(16) Mohammad Hejazi. Title: Brigadier General. Function: Commander of Bassij resistance force.

Date of UN designation: 24.3.2007. 02012R0267 — EN — 18.01.2017 — 022.003 — 264

▼B (17) Mohsen Hojati. Function: Head of Fajr Industrial Group.

Date of UN designation: 24.3.2007.

▼M25 ______

▼B (20) Mehrdada Akhlaghi Ketabachi. Function: Head of Shahid Bagheri Industrial Group (SBIG).

Date of UN designation: 24.3.2007.

▼M25 ______

▼B (22) Naser Maleki. Function: Head of Shahid Hemmat Industrial Group (SHIG). Other information: Naser Maleki is also a MODAFL official overseeing work on the Shahab-3 ballistic missile programme. The Shahab-3 is Iran's long-range ballistic missile currently in service.

Date of UN designation: 24.3.2007.

▼M25 ______

▼B (26) Mohammad Reza Naqdi. Title: Brigadier General. Other information: former Deputy Chief of Armed Forces General Staff for Logistics and Industrial Research/Head of State Anti-Smuggling Headquarters, engaged in efforts to get round the sanctions imposed by UNSCR 1737 (2006) and 1747 (2007).

Date of UN designation: 3.3.2008.

▼M25 ______

▼B (28) Mohammad Mehdi Nejad Nouri. Title: Lt Gen. Function: Rector of Malek Ashtar University of Defence Technology. Other information: The chemistry department of Ashtar University of Defence Technology is affiliated to MODALF and has conducted experiments on beryllium. Person involved in Iran's nuclear programme.

Date of UN designation: 23.12.2006.

▼M25 ______

▼B (33) Morteza Rezaie. Title: Brigadier General. Function: Deputy Commander of IRGC.

Date of UN designation: 24.3.2007.

(34) Morteza Safari. Title: Rear Admiral. Function: Commander of IRGC Navy.

Date of UN designation: 24.3.2007.

(35) Yahya Rahim Safavi. Title: Maj Gen. Function: Commander, IRGC (Pasdaran). Other information: Person involved in both Iran's nuclear and ballistic missile programmes.

Date of UN designation: 23.12.2006. 02012R0267 — EN — 18.01.2017 — 022.003 — 265

▼M25 ______

▼B (37) Hosein Salimi. Title: General. Function: Commander of the Air Force, IRGC (Pasdaran). Other information: Person involved in Iran's ballistic missile programme.

Date of UN designation: 23.12.2006.

(38) Qasem Soleimani. Title: Brigadier General. Function: Commander of Qods force.

Date of UN designation: 24.3.2007.

▼M25 ______

▼B (40) Mohammad Reza Zahedi. Title: Brigadier General. Function: Commander of IRGC Ground Forces.

Date of UN designation: 24.3.2007.

(41) General Zolqadr. Function: Deputy Interior Minister for Security Affairs, IRGC officer.

Date of UN designation: 24.3.2007.

▼M3 (42) Azim Aghajani (also spelled: Adhajani). Function: Member of the IRGC-Qods Force operating under the direction of Qods Force Commander, Major General Qasem Soleimani, who was designated by the UN Security Council in Resolution 1747 (2007).

Other information: facilitated a breach of paragraph 5 of Resolution 1747 (2007) prohibiting the export of arms and related materiel from Iran.

Additional information: Nationality: Iran. Passport Number: 6620505, 9003213

Date of UN designation: 18 April 2012.

(43) Ali Akbar Tabatabaei (alias: Sayed Akbar Tahmaesebi). Function: Member of the IRGC Qods Force operating under the direction of Qods Force Commander, Major General Qasem Soleimani, who was designated by the UN Security Council in Resolution 1747 (2007).

Other information: facilitated a breach of paragraph 5 of Resolution 1747 (2007) prohibiting the export of arms and related materiel from Iran.

Additional information: Nationality: Iran. Date of birth: 1967

Date of UN designation: 18 April 2012.

▼B Entities

(1) Abzar Boresh Kaveh Co. (alias BK Co.). Other information: involved in the production of centrifuge components.

Date of UN designation: 3.3.2008. 02012R0267 — EN — 18.01.2017 — 022.003 — 266

▼B (2) Amin Industrial Complex: Amin Industrial Complex sought temperature controllers which may be used in nuclear research and operational/pro duction facilities. Amin Industrial Complex is owned or controlled by, or acts on behalf of, the Defense Industries Organization (DIO), which was designated in resolution 1737 (2006).

Location: P.O. Box 91735-549, Mashad, Iran; Amin Industrial Estate, Khalage Rd., Seyedi District, Mashad, Iran; Kaveh Complex, Khalaj Rd., Seyedi St., Mashad, Iran

A.K.A.: Amin Industrial Compound and Amin Industrial Company.

Date of UN designation: 9.6.2010.

(3) Ammunition and Metallurgy Industries Group (alias (a) AMIG, (b) Ammunition Industries Group). Other information: (a) AMIG controls 7th of Tir, (b) AMIG is owned and controlled by the Defence Industries Organisation (DIO).

Date of UN designation: 24.3.2007.

(4) Armament Industries Group: Armament Industries Group (AIG) manu facturers and services a variety of small arms and light weapons, including large- and medium-calibre guns and related technology. AIG conducts the majority of its procurement activity through Hadid Industries Complex.

Location: Sepah Islam Road, Karaj Special Road Km 10, Iran; Pasdaran Ave., P.O. Box 19585/777, Tehran, Iran.

Date of EU designation: 24.4.2007 (UN: 9.6.2010).

▼M25 ______

▼M28 ______

▼B (7) Barzagani Tejarat Tavanmad Saccal companies. Other information: (a) subsidiary of Saccal System companies, (b) this company tried to purchase sensitive goods for an entity listed in resolution 1737 (2006).

Date of UN designation: 3.3.2008.

(8) Cruise Missile Industry Group (alias Naval Defence Missile Industry Group).

Date of UN designation: 24.3.2007.

(9) Defence Industries Organisation (DIO). Other information: (a) Over arching MODAFL-controlled entity, some of whose subordinates have been involved in the centrifuge programme making components, and in the missile programme, (b) Involved in Iran's nuclear programme.

Date of UN designation: 23.12.2006. 02012R0267 — EN — 18.01.2017 — 022.003 — 267

▼B (10) Defense Technology and Science Research Center: Defense Technology and Science Research Center (DTSRC) is owned or controlled by, or acts on behalf of, Iran's Ministry of Defense and Armed Forces Logistics (MODAFL), which oversees Iran's defence R&D, production, maintenance, exports, and procurement.

Location: Pasdaran Ave, PO Box 19585/777, Tehran, Iran.

Date of EU designation: 24.4.2007 (UN: 9.6.2010).

(11) Doostan International Company: Doostan International Company (DICO) supplies elements to Iran's ballistic missile program.

Date of UN designation: 9.6.2010.

(12) Electro Sanam Company (alias (a) E. S. Co., (b) E. X. Co.). Other information: AIO front-company, involved in the ballistic missile programme.

Date of UN designation: 3.3.2008.

▼M25 ______

▼B (14) Ettehad Technical Group. Other information: AIO front-company, involved in the ballistic missile programme.

Date of UN designation: 3.3.2008.

(15) Fajr Industrial Group. Other information: (a) Formerly Instrumentation Factory Plant, (b) Subordinate entity of AIO, (c) Involved in Iran's ballistic missile programme.

Date of UN designation: 23.12.2006.

(16) Farasakht Industries: Farasakht Industries is owned or controlled by, or act on behalf of, the Iran Aircraft Manufacturing Company, which in turn is owned or controlled by MODAFL.

Location: P.O. Box 83145-311, Kilometer 28, Esfahan-Tehran Freeway, Shahin Shahr, Esfahan, Iran.

Date of UN designation: 9.6.2010.

(17) Farayand Technique. Other information: (a) Involved in Iran's nuclear programme (centrifuge programme), (b) Identified in IAEA reports.

Date of UN designation: 23.12.2006.

▼M25 ______02012R0267 — EN — 18.01.2017 — 022.003 — 268

▼B (19) Industrial Factories of Precision (IFP) Machinery (alias Instrumentation Factories Plant). Other information: used by AIO for some acquisition attempts.

Date of UN designation: 3.3.2008.

▼M25 ______

▼B (21) Joza Industrial Co. Other information: AIO front-company, involved in the ballistic missile programme.

Date of UN designation: 3.3.2008.

(22) Kala-Electric (alias Kalaye Electric). Other information: (a) Provider for PFEP - Natanz, (b) Involved in Iran's nuclear programme.

Date of UN designation: 23.12.2006.

▼M25 ______

▼B (24) Kaveh Cutting Tools Company: Kaveh Cutting Tools Company is owned or controlled by, or acts on behalf of, the DIO.

Location: 3rd Km of Khalaj Road, Seyyedi Street, Mashad 91638, Iran; Km 4 of Khalaj Road, End of Seyedi Street, Mashad, Iran; P.O. Box 91735-549, Mashad, Iran; Khalaj Rd., End of Seyyedi Alley, Mashad, Iran; Moqan St., Pasdaran St., Pasdaran Cross Rd., Tehran, Iran.

Date of UN designation: 9.6.2010.

▼M25 ______

▼B (26) Khorasan Metallurgy Industries. Other information: (a) subsidiary of the Ammunition Industries Group (AMIG) which depends on DIO, (b) involved in the production of centrifuge components.

Date of UN designation: 3.3.2008.

(27) M. Babaie Industries: M. Babaie Industries is subordinate to Shahid Ahmad Kazemi Industries Group (formally the Air Defense Missile Industries Group) of Iran's Aerospace Industries Organization (AIO). AIO controls the missile organizations Shahid Hemmat Industrial Group (SHIG) and the Shahid Bakeri Industrial Group (SBIG), both of which were designated in resolution 1737 (2006).

Location: P.O. Box 16535-76, Tehran, 16548, Iran.

Date of UN designation: 9.6.2010.

(28) Malek Ashtar University: A subordinate of the DTRSC within MODAFL. This includes research groups previously falling under the Physics Research Center (PHRC). IAEA inspectors have not been allowed to interview staff or see documents under the control of this organization to resolve the outstanding issue of the possible military dimension to Iran's nuclear program.

Location: Corner of Imam Ali Highway and Babaei Highway, Tehran, Iran.

Date of EU designation: 24.6.2008 (UN: 9.6.2010). 02012R0267 — EN — 18.01.2017 — 022.003 — 269

▼M25 ______

▼B (30) Ministry of Defense Logistics Export: Ministry of Defense Logistics Export (MODLEX) sells Iranian-produced arms to customers around the world in contravention of resolution 1747 (2007), which prohibits Iran from selling arms or related materiel.

Location: PO Box 16315-189, Tehran, Iran; located on the west side of Dabestan Street, Abbas Abad District, Tehran, Iran.

Date of EU designation: 24.6.2008 (UN: 9.6.2010).

(31) Mizan Machinery Manufacturing: Mizan Machinery Manufacturing (3M) is owned or controlled by, or acts on behalf of, SHIG.

Location: P.O. Box 16595-365, Tehran, Iran

A.K.A.: 3MG

Date of EU designation: 24.6.2008 (UN: 9.6.2010).

▼M25 ______

▼B (34) Niru Battery Manufacturing Company. Other information: (a) subsidiary of the DIO, (b) its role is to manufacture power units for the Iranian military including missile systems.

Date of UN designation: 3.3.2008.

▼M25 ______

▼B (36) Parchin Chemical Industries. Other information: Branch of DIO.

Date of UN designation: 24.3.2007.

(37) Pars Aviation Services Company. Other information: maintains aircraft.

Date of UN designation: 24.3.2007.

▼M25 ______

▼B (39) Pejman Industrial Services Corporation: Pejman Industrial Services Corporation is owned or controlled by, or acts on behalf of, SBIG.

Location: P.O. Box 16785-195, Tehran, Iran.

Date of UN designation: 9.6.2010.

▼M25 ______

▼B (41) Qods Aeronautics Industries. Other information: It produces unmanned aerial vehicles (UAVs), parachutes, paragliders, paramotors, etc.

Date of UN designation: 24.3.2007.

(42) Sabalan Company: Sabalan is a cover name for SHIG.

Location: Damavand Tehran Highway, Tehran, Iran.

Date of UN designation: 9.6.2010.

(43) Sanam Industrial Group. Other information: subordinate to AIO.

Date of UN designation: 24.3.2007. 02012R0267 — EN — 18.01.2017 — 022.003 — 270

▼B (44) Safety Equipment Procurement (SEP). Other information: AIO front- company, involved in the ballistic missile programme.

Date of UN designation: 3.3.2008.

(45) 7th of Tir. Other information: (a) Subordinate of DIO, widely recognised as being directly involved in Iran's nuclear programme, (b) Involved in Iran's nuclear programme.

Date of UN designation: 23.12.2006.

(46) Sahand Aluminum Parts Industrial Company (SAPICO): SAPICO is a cover name for SHIG.

Location: Damavand Tehran Highway, Tehran, Iran.

Date of UN designation: 9.6.2010.

(47) Shahid Bagheri Industrial Group (SBIG). Other information: (a) Subordinate entity of AIO, (b) Involved in Iran's ballistic missile programme.

Date of UN designation: 23.12.2006.

(48) Shahid Hemmat Industrial Group (SHIG). Other information: (a) subordinate entity of AIO, (b) Involved in Iran's ballistic missile programme.

Date of UN designation: 23.12.2006.

(49) Shahid Karrazi Industries: Shahid Karrazi Industries is owned or controlled by, or act on behalf of, SBIG.

Location: Tehran, Iran.

Date of UN designation: 9.6.2010.

(50) Shahid Satarri Industries: Shahid Sattari Industries is owned or controlled by, or acts on behalf of, SBIG.

Location: Southeast Tehran, Iran

A.K.A.: Shahid Sattari Group Equipment Industries.

Date of UN designation: 9.6.2010.

(51) Shahid Sayyade Shirazi Industries: Shahid Sayyade Shirazi Industries (SSSI) is owned or controlled by, or acts on behalf of, the DIO.

Location: Next To Nirou Battery Mfg. Co, Shahid Babaii Expressway, Nobonyad Square, Tehran, Iran; Pasdaran St., P.O. Box 16765, Tehran 1835, Iran; Babaei Highway — Next to Niru M.F.G, Tehran, Iran.

Date of UN designation: 9.6.2010.

(52) Sho'a' Aviation. Other information: It produces microlights.

Date of UN designation: 24.3.2007.

(53) Special Industries Group: Special Industries Group (SIG) is a subordinate of DIO.

Location: Pasdaran Avenue, PO Box 19585/777, Tehran, Iran.

Date of EU designation: 24.7.2007 (UN: 9.6.2010). ▼M25 ______

▼B (55) Tiz Pars: Tiz Pars is a cover name for SHIG. Between April and July 2007, Tiz Pars attempted to procure a five axis laser welding and cutting machine, which could make a material contribution to Iran's missile program, on behalf of SHIG.

Location: Damavand Tehran Highway, Tehran, Iran.

Date of UN designation: 9.6.2010. 02012R0267 — EN — 18.01.2017 — 022.003 — 271

▼B (56) Ya Mahdi Industries Group. Other information: subordinate to AIO.

Date of UN designation: 24.3.2007.

(57) Yazd Metallurgy Industries: Yazd Metallurgy Industries (YMI) is a subordinate of DIO.

Location: Pasdaran Avenue, Next To Telecommunication Industry, Tehran 16588, Iran; Postal Box 89195/878, Yazd, Iran; P.O. Box 89195-678, Yazd, Iran; Km 5 of Taft Road, Yazd, Iran.

A.K.A.: Yazd Ammunition Manufacturing and Metallurgy Industries, Directorate of Yazd Ammunition and Metallurgy Industries

Date of UN designation: 9.6.2010.

▼M3 (58) Behineh Trading Co.

Other information: An Iranian company that played a key role in Iran’s illicit transfer of arms to West Africa and acted on behalf of the IRGC Qods Force, commanded by Major General Qasem Soleimani, designated by the UN Security Council in Resolution 1747 (2007), as the shipper of the weapons consignment.

Additional information: Location: Tavakoli Building, Opposite of 15th Alley, Emam-Jomeh Street, Tehran, Iran. Telephone: +98 9195382305. Website: http://www.behinehco.ir

Date of UN designation: 18 April 2012.

▼M9 (59) Yas Air: Yas Air is the new name for Pars Air, a company that was owned by Pars Aviation Services Company, which in turn was designated by the United Nations Security Council in Resolution 1747 (2007). Yas Air has assisted Pars Aviation Services Company, a United Nations-designated entity, in violating paragraph 5 of Resolution 1747 (2007).

Location: Mehrabad International Airport, Next to Terminal No. 6, Tehran, Iran.

Date of UN designation: 10.12.2012.

(60) SAD Import Export Company: SAD Import Export Company has assisted Parchin Chemical Industries and 7th of Tir Industries, a United Nations-designated entity, in violating paragraph 5 of Resolution 1747 (2007).

Location: Haftom Tir Square, South Mofte Avenue, Tour Line No 3/1, Tehran, Iran. (2) P.O. Box 1584864813.

Date of UN designation: 10.12.2012.

▼B B. Entities owned, controlled, or acting on behalf of the ►C1 Iranian Revolutionary Guard Corps ◄

(1) Fater (or Faater) Institute: Khatam al-Anbiya (KAA) subsidiary. Fater has worked with foreign suppliers, likely on behalf of other KAA companies on IRGC projects in Iran.

Date of UN designation: 9.6.2010.

(2) Gharagahe Sazandegi Ghaem: Gharagahe Sazandegi Ghaem is owned or controlled by KAA

Date of UN designation: 9.6.2010. 02012R0267 — EN — 18.01.2017 — 022.003 — 272

▼B (3) Ghorb Karbala: Ghorb Karbala is owned or controlled by KAA. Date of UN designation: 9.6.2010. (4) Ghorb Nooh: Ghorb Nooh is owned or controlled by KAA. Date of UN designation: 9.6.2010. (5) Hara Company: Owned or controlled by Ghorb Nooh. Date of UN designation: 9.6.2010. (6) Imensazan Consultant Engineers Institute: Owned or controlled by, or acts on behalf of, KAA. Date of UN designation: 9.6.2010. (7) Khatam al-Anbiya Construction Headquarters: Khatam al-Anbiya Construction Headquarters (KAA) is an IRGC-owned company involved in large scale civil and military construction projects and other engineering activities. It undertakes a significant amount of work on Passive Defense Organization projects. In particular, KAA subsidiaries were heavily involved in the construction of the uranium enrichment site at Qom/Fordow. Date of UN designation: 9.6.2010. (8) Makin: Makin is owned or controlled by or acting on behalf of KAA, and is a subsidiary of KAA. Date of UN designation: 9.6.2010. (9) Omran Sahel: Owned or controlled by Ghorb Nooh. Date of UN designation: 9.6.2010. (10) Oriental Oil Kish: Oriental Oil Kish is owned or controlled by or acting on behalf of KAA. Date of UN designation: 9.6.2010. (11) Rah Sahel: Rah Sahel is owned or controlled by or acting on behalf of KAA. Date of UN designation: 9.6.2010. (12) Rahab Engineering Institute: Rahab is owned or controlled by or acting on behalf of KAA, and is a subsidiary of KAA. Date of UN designation: 9.6.2010. (13) Sahel Consultant Engineers: Owned or controlled by Ghorb Nooh. Date of UN designation: 9.6.2010. (14) Sepanir: Sepanir is owned or controlled by or acting on behalf of KAA. Date of UN designation: 9.6.2010. (15) Sepasad Engineering Company: Sepasad Engineering Company is owned or controlled by or acting on behalf of KAA. Date of UN designation: 9.6.2010. C. Entities owned, controlled, or acting on behalf of the Islamic Republic of Iran Shipping Lines (IRISL) ▼M25 ______02012R0267 — EN — 18.01.2017 — 022.003 — 273

▼B ANNEX IX

List of persons and entities referred to in Article 23(2) I. ►M4 Persons and entities involved in nuclear or ballistic missile activities and persons and entities providing support to the Government of Iran ◄

A. Persons

Name Identifying information Reasons Date of listing

▼M25 _____

▼M3 _____

▼M25 _____

▼B

4. Engineer Mojtaba MODAFL Deputy for Industry. 23.6.2008 HAERI Supervisory role over AIO and DIO

▼M21 _____

▼M25 _____

▼B

8. Ebrahim Managing Director of Iran Electronic 23.6.2008 MAHMUDZADEH Industries (see Part B, no 20)

▼M14 _____

▼B

10. Brigadier-General Beik MODAFL Deputy for Supplies and 23.6.2008 MOHAMMADLU Logistics (see Part B, no 29)

▼M4 _____

▼B

12. Mohammad Reza Head of Samen Al A'Emmeh Industries 26.7.2010 MOVASAGHNIA Group (SAIG), also known as the Cruise Missile Industry Group. This organisation was designated under UNSCR 1747 and listed in Annex I to Common Position 2007/140/CFSP.

13. Anis NACCACHE Administrator of Barzagani Tejarat 23.6.2008 Tavanmad Saccal companies; his company has attempted to procure sensitive goods for entities designated under Resolution 1737 (2006). 02012R0267 — EN — 18.01.2017 — 022.003 — 274

▼B

Name Identifying information Reasons Date of listing

14. Brigadier-General Head of Aerospace Industries 23.6.2008 Mohammad NADERI Organisation (AIO) (see Part B, no 1). AIO has taken part in sensitive Iranian programmes.

▼M25 _____

▼B

16. Rear Admiral Former MODAFL Deputy for 23.6.2008 Mohammad SHAFI'I Coordination (see Part B, no 29). RUDSARI

17. Abdollah SOLAT SANA Managing Director of the Uranium 23.4.2007 Conversion Facility (UCF) in Esfahan. This is the facility that produces the feed material (UF6) for the enrichment facilities at Natanz. On 27 August 2006, Solat Sana received a special award from President Ahmadinejad for his role.

▼M25 _____

▼M3 _____

▼B

23. Davoud BABAEI The current head of security for the 1.12.2011 Ministry Of Defence Armed Forces Logistics' research institute the Organisation of Defensive Innovation and Research (SPND), which is run by UN designated Mohsen Fakhrizadeh. The IAEA have identified SPND with their concerns over possible military dimensions to Iran's nuclear programme over which Iran refuses to co-operate. As head of security, Babaei is responsible for preventing the disclosure of information including to the IAEA.

▼M4 _____

▼B

25. Sayed Shamsuddin Deputy Head of UN designated Atomic 1.12.2011 BORBORUDI Energy Organisation of Iran, where he is subordinate to UN designated Feridun Abbasi Davani. Has been involved in the Iranian nuclear programme since at least 2002, including as the former head of procurement and logistics at AMAD, where he was responsible for using front companies such as Kimia Madan to procure equipment and material for Iran's nuclear weapons programme. 02012R0267 — EN — 18.01.2017 — 022.003 — 275

▼B

Name Identifying information Reasons Date of listing

▼M4 _____

▼B

27. Kamran DANESHJOO Minister of Science, Research and 1.12.2011 (a.k.a. DANESHJOU) Technology since the 2009 election. Iran failed to provide the IAEA with clarification of his role in relation to missile warhead development studies. This is part of Iran's wider non- cooperation with the IAEA investigation of the 'Alleged Studies' suggesting a military aspect to Iran's nuclear programme, which includes denial of access to relevant individuals associated documents. Daneshjoo also plays a role in 'Passive Defence' activities on behalf of President Ahmadenijad, in addition to his ministerial role. The Passive Defence Organisation is already EU designated.

▼M3 _____

▼B

29. Milad JAFARI date of birth 20.9.74 An Iranian national supplying goods, 1.12.2011 mostly metals, to UN designated SHIG front companies. Delivered goods to SHIG between January and November 2010. Payments for some of the goods were made at the central branch of EU- designated Export Development Bank of Iran (EDBI) in Tehran after November 2010.

▼M4 _____

▼B

31. Ali KARIMIAN An Iranian national supplying goods, 1.12.2011 mostly carbon fibre to UN-designated SHIG and SBIG.

32. Majid KHANSARI Managing Director of UN-designated 1.12.2011 Kalaye Electric Company.

▼M4 _____

▼M3 _____

▼B

35. Mohammad Managing Director of MATSA. 1.12.2011 MOHAMMADI 02012R0267 — EN — 18.01.2017 — 022.003 — 276

▼B

Name Identifying information Reasons Date of listing ▼M4 _____

▼B

37. Mohammad Sadegh Head of the Physics Research Institute 1.12.2011 NASERI (formerly known as the Institute of Applied Physics). ▼M25 _____

▼M1 _____

▼B

40. Hamid SOLTANI Managing Director of the EU-designated 1.12.2011 Management Company for Nuclear Power Plant Construction (MASNA) ▼M4 _____

▼B

42. Javad AL YASIN Head of the Research Centre for 1.12.2011 Explosion and Impact, also known as METFAZ ▼M3 _____

▼M25 _____

▼B B. Entities

Name Identifying information Reasons Date of listing

1. Aerospace Industries AIO, 28 Shian 5, Lavizan, AIO oversees Iran's production of 23.4.2007 Organisation, AIO Tehran, Iran missiles, including Shahid Hemmat Langare Street,Nobonyad Square, Industrial Group, Shahid Bagheri Tehran, Iran Industrial Group and Fajr Industrial Group, which were all designated under UNSCR 1737 (2006). The head of AIO and two other senior officials were also designated under UNSCR 1737 (2006) 2. Armed Forces Assessed to provide geospatial data for 23.6.2008 Geographical Organi the Ballistic Missile programme sation ▼M25 _____

▼B ______4. ►M25 ◄ ►M25 ◄ ►M25 ◄ ►M25 ◄ ______►M25 ◄ ►M25 ◄ ►M25 ◄ ►M25 ◄ (b) ██████ ██████ ██████ ██████ ▼M25 _____

▼B 6. ██████ ██████ ██████ ██████ 02012R0267 — EN — 18.01.2017 — 022.003 — 277

▼B

Name Identifying information Reasons Date of listing

7. ██████ ███████ ██████ ██████

▼M31 _____

▼M29

7a. (1 ) ██████ ███████ ██████

______►M29 ◄ ►M29 ◄ ►M29 ◄

▼M25 _____

▼B

9. ESNICO (Equipment No. 1, 37th Avenue, Asadabadi Procures industrial goods, specifically for 26.7.2010 Supplier for Nuclear Street, Tehran, Iran the nuclear programme activities carried Industries Corporation) out by AEOI, Novin Energy and Kalaye Electric Company (all designated under UNSCR 1737). ESNICO's Director is Haleh Bakhtiar (designated in UNSCR 1803).

10. Etemad Amin Invest Pasadaran Av. Tehran, Iran Close to Naftar and to Bonyad-e Mosta 26.7.2010 Co Mobin zafan, Etemad Amin Invest Co Mobin contributes to funding the strategic interests of the regime and of the parallel Iranian state.

11. ██████ ██████ ████████████ ██████ ██████ ██████ ██████ ██████ ██████

███ ██████ ██████ ██████ ██████ ██████ ██████

███ ██████ ██████ ██████ ██████

12. Fajr Aviation Mehrabad Airport, PO Box A subsidiary of the IAIO within 26.7.2010 Composite Industries 13445-885, Tehran, Iran MODAFL (see no 29), which primarily produces composite materials for the aircraft industry, but also linked to the development of carbon fibre capabilities for nuclear and missile applications. Linked to the Technology Cooperation Office. Iran has recently announced its intention to mass produce new generation centrifuges which will require FACI carbon fibre production capabilities. 02012R0267 — EN — 18.01.2017 — 022.003 — 278

▼B

Name Identifying information Reasons Date of listing

▼M14 _____

▼M25 _____

▼B

16. Iran Aircraft Industries A subsidiary of the IAIO within 26.7.2010 (IACI) MODAFL (see no 29). Manufactures, repairs, and conducts overhauls of airplanes and aircraft engines and procures aviation-related parts often of US-origin typically via foreign intermedi aries. IACI and its subsidiaries have also been detected using a worldwide network of brokers seeking to procure aviation- related goods.

17. Iran Aircraft Manufac P.O. Box 83145-311, 28 km Owned or controlled by, or acts on behalf 26.7.2010 turing Company (a.k.a: Esfahan – Tehran Freeway, of; MODAFL (see no 29). HESA, HESA Trade Shahin Shahr, Esfahan, Iran; Center, HTC, IAMCO, P.O. Box 14155-5568, No. 27 IAMI, Iran Aircraft Ahahamat Ave., Vallie Asr Manufacturing Square, Tehran 15946, Iran; Company, Iran P.O. Box 81465-935, Esfahan, Aircraft Manufacturing Iran; Industries, Kark Shahih Shar Industrial Zone, hanejate Sanaye Isfahan, Iran; P.O. Box 8140, Havapaymaie Iran, No. 107 Sepahbod Gharany Hava Peyma Sazi-e Ave., Tehran, Iran Iran, Havapeyma Sazhran, Havapeyma Sazi Iran, Hevapei masazi)

18. Iran Centrifuge Tech 156 Golestan Street, Saradr-e Iran Centrifuge Technology Company has 26.07.2010 nology Company Jangal, Tehran taken over the activities of Farayand (a.k.a. TSA or TESA) Technique (designated under UNSCR 1737). It manufactures uranium enrichment centrifuge parts, and is directly supporting proliferation sensitive activity that Iran is required to suspend by UNSCRs. Carries out work for Kalaye Electric Company (designated under UNSCR 1737).

19. Iran Communications PO Box 19295-4731, Pasdaran Iran Communications Industries, a 26.7.2010 Industries (ICI) Avenue, Tehran, Iran; subsidiary of Iran Electronics Industries Alternative address: (see no 20), produces various items PO Box 19575-131, 34 Apadana including communication systems, Avenue, Tehran, Iran; avionics, optics and electro-optics Alternative address: devices, micro-electronics, information technology, test and measurement, tele Shahid Langary Street, Nobonyad communication security, electronic Square Ave, Pasdaran, Tehran warfare, radar tube manufacture and refurbishment, and missile launchers. These items can be used in programmes that are under sanction per UNSCR 1737. 02012R0267 — EN — 18.01.2017 — 022.003 — 279

▼B

Name Identifying information Reasons Date of listing

20. Iran Electronics P. O. Box 18575-365, Tehran, Wholly-owned subsidiary of MODAFL 23.6.2008 Industries Iran (and therefore a sister-organisation to (including all AIO, AvIO and DIO). Its role is to manu branches) and subsidi facture electronic components for Iranian aries: weapons systems.

(a) Isfahan Optics P.O. Box 81465-313 Kaveh Ave. Owned, controlled by, or acts on behalf 26.7.2010 Isfahan - Iran of Iran Electronics Industries P.O. Box 81465-117, Isfahan, Iran

21. ██████ ██████ ██████ ██████ ██████

22. Iranian Aviation Ave. Sepahbod Gharani P.O. Box A MODAFL (see no 29) organisation 26.7.2010 Industries Organ 15815/1775 Tehran, Iran responsible for planning and managing ization (IAIO) Ave. Sepahbod Gharani P.O. Box Iran's military aviation industry. 15815/3446 Tehran, Iran 107 Sepahbod Gharani Avenue, Tehran, Iran

23. Javedan Mehr Toos Engineering firm that procures for the 26.7.2010 Atomic Energy Organisation of Iran which was designated under UNSCR 1737.

▼M25 _____

▼B

26. Marine Industries Pasdaran Av., PO Box 19585/ A subsidiary of the DIO 23.4.2007 777, Tehran

▼M25 _____

▼B

28. Mechanic Industries Took part in the production of 23.6.2008 Group components for the ballistics programme.

29. Ministry Of Defense Located on the west side of Responsible for Iran's defence research, 23.06.2008 And Support For Dabestan Street, Abbas Abad development and manufacturing Armed Forces District, Tehran, Iran programmes, including support to Logistics (a.k.a. missile and nuclear programmes. Ministry Of Defense For Armed Forces Logistics; a.k.a. MODAFL; a.k.a. MODSAF)

▼M25 _____

▼B

31. Parchin Chemical Worked on propulsion techniques for the 23.6.2008 Industries Iranian ballistics programme.

32. Parto Sanat Co No. 1281 Valiasr Ave., Next to Manufacturer of frequency changers and 26.7.2010 14th St., Tehran, 15178 Iran. it is capable of developing/modifying imported foreign frequency changers in a way that makes them usable in gas centrifuge enrichment. It is deemed to be involved in nuclear proliferation activ ities. 02012R0267 — EN — 18.01.2017 — 022.003 — 280

▼B

Name Identifying information Reasons Date of listing

33. Passive Defense Responsible for the selection and 26.7.2010 Organization construction of strategic facilities, including – according to Iranian statements - the uranium enrichment site at Fordow (Qom) built without being declared to the IAEA contrary to Iran's obligations (affirmed in a resolution by the IAEA Board of Governors). Brigadier General Gholam-Reza Jalali, former IRGC is PDO's chairman.

34. ██████ ██████ ██████ ██████

35. Raka A department of Kalaye Electric 26.7.2010 Company (designated under UNSCR 1737). Established in late 2006, it was responsible for the construction of the Uranium enrichment plant at Fordow (Qom).

▼M25 _____

▼B

37. Schiller Novin Gheytariyeh Avenue - no 153 - Acting on behalf of Defense Industries 26.7.2010 3rd Floor - PO BOX 17665/153 Organisation (DIO). 6 19389 Teheran

38. Shahid Ahmad SAKIG develops and produces surface-to- 26.7.2010 Kazemi Industrial air missiles systems for Iran's military. It Group maintains military, missile, and air defense projects and procures goods from Russia, Belarus, and North Korea.

39. Shakhese Behbud Involved in the production of equipment 26.7.2010 Sanat and parts for the nuclear fuel cycle.

40. State Purchasing The SPO appears to facilitate the import 23.6.2008 Organisation (SPO) of whole weapons. It appears to be a subsidiary of MODAFL 02012R0267 — EN — 18.01.2017 — 022.003 — 281

▼B

Name Identifying information Reasons Date of listing

▼M8

41. Technology Tehran, Iran Responsible for Iran's technological 26.07.2010 Cooperation Office advancement through relevant foreign (TCO) of the Iranian procurement and training links. Supports President's Office the nuclear and missile programmes. (a.k.a. Center for Innovation and Technology (CITC))

42. Yasa Part, (including Company dealing with procurement 26.7.2010 all branches) and activities related to the purchase of subsidiaries: materials and technologies necessary to nuclear and ballistic programmes.

(a) Arfa Paint Acting on behalf of Yasa Part. 26.7.2010 Company

(b) Arfeh Company Acting on behalf of Yasa Part. 26.7.2010

(d) Hosseini Nejad Acting on behalf of Yasa Part. 26.7.2010 Trading Co.

(e) Iran Saffron Acting on behalf of Yasa Part. 26.7.2010 Company or Iransaffron Co.

(f) Shetab G. Acting on behalf of Yasa Part. 26.7.2010

(g) Shetab Gaman Acting on behalf of Yasa Part. 26.7.2010

(h) Shetab Trading Acting on behalf of Yasa Part. 26.7.2010

(i) Y.A.S. Co. Ltd Acting on behalf of Yasa Part. 26.7.2010

▼M25 _____

▼B

45. Aras Farayande Unit 12, No 35 Kooshesh Street, Involved in procurement of materials for 23.05.2011 Tehran EU-sanctioned Iran Centrifuge Technology Company

▼M25 _____

▼B

47. Neda Industrial Group No 10 & 12, 64th Street, Yusef Industrial automation company that has 23.05.2011 Abad, Tehran worked for the UN-sanctioned Kalaye Electric Company (KEC) at the uranium fuel enrichment plant at Natanz.

▼M31 _____

▼B

49. Noavaran Pooyamoj No 15, Eighth Street, Pakistan Involved in procurement of materials that 23.05.2011 Avenue, Shahid Beheshti are controlled and have direct application Avenue, Tehran in the manufacture of centrifuges for Iran's uranium enrichment programme. 02012R0267 — EN — 18.01.2017 — 022.003 — 282

▼B

Name Identifying information Reasons Date of listing

▼M25 _____

▼M4 _____

▼B

52. Raad Iran (a.k.a Raad Unit 1, No 35, Bouali Sina A company involved in procurement of 23.05.2011 Automation Company) Sharghi, Chehel Sotoun Street, inverters for Iran's proscribed enrichment Fatemi Square, Tehran programme. RaadIran was established to produce and design controlling systems and provides the sale and installation of inverters and programmable Logic Controllers.

▼M25 _____

▼B

54. Sun Middle East FZ A company that procures sensitive goods 23.05.2011 Company for the Nuclear Reactors Fuel Company (SUREH). Sun Middle East uses inter mediaries based outside of Iran to source goods SUREH requires. Sun Middle East provides these intermediaries with false end user details for when the goods are sent to Iran, thereby seeking to circumvent the relevant country's Customs regime.

55. Ashtian Tablo Ashtian Tablo - No 67, Ghods A manufacturer of electrical equipment 23.05.2011 mirheydari St, Yoosefabad, (switchgear)involved in the construction Tehran of the Fordow (Qom) facility, built without being declared to the IAEA.

56. Bals Alman A manufacturer of electrical equipment 23.05.2011 (switchgear) involved in the ongoing construction of the Fordow (Qom) facility built without being declared to the IAEA.

57. Hirbod Co Hirbod Co - Flat 2, 3 Second A company that has procured goods and 23.05.2011 Street, Asad Abadi Avenue, equipment destined for Iran's Nuclear and Tehran 14316 Ballistic Missile programmes for the UN- sanctioned Kalaye Electric Company (KEC).

▼M13 _____

▼B

59. Marou Sanat (a.k.a. 9, Ground Floor, Zohre Street, Procurement firm that has acted for 23.05.2011 Mohandesi Tarh Va Mofateh Street, Tehran Mesbah Energy which was designated Toseh Maro Sanat under UNSCR 1737 Company)

60. Paya Parto (a.k.a. Paya Subsidiary of Novin Energy, which was 23.05.2011 Partov) sanctioned under UNSCR 1747, involved in laser welding. 02012R0267 — EN — 18.01.2017 — 022.003 — 283

▼B

Name Identifying information Reasons Date of listing

▼M16 _____

▼B

62. Taghtiran Engineering firm that procures equipment 23.05.2011 for Iran's IR-40 heavy water research reactor

▼M25 _____

▼M31 _____

▼B

66. MAAA Synergy Malaysia Involved in procurement of components 23.05.2011 for Iranian fighter planes

67. Modern Technologies PO Box 8032, Sharjah, United Involved in procurement of components 23.05.2011 FZC (MTFZC) Arab Emirates for Iranian nuclear programme

68. ██████ ██████ ██████ ██████

▼M25 _____

▼B

70. Tajhiz Sanat Shayan Unit 7, No. 40, Yazdanpanah, Involved in procurement of components 23.05.2011 (TSS) Afriqa Blvd., Teheran, Iran for Iranian nuclear programme

71. Institute of Applied Conducts research into military 23.05.2011 Physics (IAP) applications of Iranian nuclear programme

72. Aran Modern Devices Affiliated to MTFZC network 23.05.2011 (AMD)

▼M13 _____

▼B

74. Electronic Hossain Abad Avenue, Shiraz, Subsidiary of Iran Electronics Industries 23.05.2011 Components Industries Iran (ECI)

75. Shiraz Electronics Mirzaie Shirazi, P.O. Box 71365- Subsidiary of Iran Electronics Industries 23.05.2011 Industries 1589, Shiraz, Iran

▼M21

76. Iran Marine Industrial Sadra Building No 3, Shafagh St., Effectively controlled by Sepanir Oil & 23.5.2011 Company (SADRA) Poonak Khavari Blvd., Shahrak Gas Energy Engineering Company, Ghods, P.O. Box 14669-56491, which is designated by the EU as an Tehran, Iran IRGC company. Provides support to the Government of Iran through its involvement in the Iranian energy sector including in the South Pars Gas field. 02012R0267 — EN — 18.01.2017 — 022.003 — 284

▼M21

Name Identifying information Reasons Date of listing

77. Shahid Beheshti Daneshju Blvd., Yaman St., Shahid Beheshti University is a public 23.5.2011 University Chamran Blvd., P.O. Box 19839- entity which is under the supervision of 63113, Tehran, Iran the Ministry of Science, Research and Technology. Carries out scientific research relevant to the development of nuclear weapons.

▼B

78. Aria Nikan, (a.k.a. Suite 1, 59 Azadi Ali North Known to procure for EU designated Iran 1.12.2011 Pergas Aria Movalled Sohrevardi Avenue, Tehran, Centrifuge Technology Company (TESA) Ltd) 1576935561 Commercial Department. They have made efforts to procure designated materials, including goods from the EU, which have applications in the Iranian nuclear programme.

79. Bargh Azaraksh; (a.k.a No 599, Stage 3, Ata Al Malek Company that has been contracted to 1.12.2011 Barghe Azerakhsh Blvd, Emam Khomeini Street, work at the uranium enrichment sites at Sakht) Esfahan. Natanz and Qom/Fordow on the elec tricity and piping works. It was in charge of designing, procuring and installing electrical control equipment at Natanz in 2010.

▼M3 _____

▼B

81. Eyvaz Technic No 3, Building 3, Shahid Hamid Producer of vacuum equipment that has 1.12.2011 Sadigh Alley, Shariati Street, supplied the uranium enrichment sites at Tehran, Iran. Natanz and Qom/Fordow. In 2011 it supplied pressure transducers to UN- designated Kalaye Electric Company.

▼M25 _____

▼B

83. Ghani Sazi Uranium 3, Qarqavol Close, 20th Street, Subordinate to the UN-designated 1.12.2011 Company (a.k.a. Iran Tehran TAMAS. It has production contracts Uranium Enrichment with UN-designated Kalaye Electric Company) Company and EU-designated TESA.

84. Iran Pooya (a.k.a. Iran A government owned company that 1.12.2011 Pouya) operated the biggest extruder of aluminium in Iran and supplied material for use in the production of casings for the IR-1 and IR-2 centrifuges. A major manufacturer of aluminium cylinders for centrifuges whose customers include the UN-designated AEOI and EU-designated TESA.

85. ██████ ██████ ██████ ██████

86. Karanir (a.k.a. Moaser, 1139/1 Unit 104 Gol Building, Involved in purchasing equipment and 1.12.2011 a.k.a. Tajhiz Sanat) Gol Alley, North Side of Sae, materials which have direct applications Vali Asr Avenue. PO Box in the Iranian nuclear programme. 19395-6439, Tehran.

87. Khala Afarin Pars Unit 5, 2nd Floor, No75, Mehran Involved in purchasing equipment and 1.12.2011 Afrand St, Sattarkhan St, Tehran. materials which have direct applications in the Iranian nuclear programme. 02012R0267 — EN — 18.01.2017 — 022.003 — 285

▼B

Name Identifying information Reasons Date of listing

88. MACPAR Makina San Istasyon MH, Sehitler cad, Company run by Milad Jafari who has 1.12.2011 Ve Tic Guldeniz Sit, Number 79/2, supplied goods, mostly metals, to UN Tuzla 34930, Istanbul designated Shahid Hemmat Industries Group (SHIG) through front companies.

89. MATSA (Mohandesi 90, Fathi Shaghaghi Street, Iranian company contracted to UN- 1.12.2011 Toseh Sokht Atomi Tehran, Iran. designated Kalaye Electric Company to Company) provide design and engineering services across the nuclear fuel cycle. Most recently has been procuring equipment for the Natanz uranium enrichment site.

▼M3

90. Mobin Sanjesh Entry 3, No 11, 12th Street, Involved in purchasing equipment and 1.12.2011 Miremad Alley, Abbas Abad, materials which have direct applications Tehran in the Iranian nuclear programme.

▼B

91. Multimat lc ve Dis Company run by Milad Jafari who has 1.12.2011 Ticaret Pazarlama supplied goods, mostly metals, to UN Limited Sirketi designated Shahid Hemmat Industries Group (SHIG) through front companies.

92. Research Centre for 44, 180th Street West, Tehran, Subordinate to the EU-designated Malek 1.12.2011 Explosion and Impact 16539-75751 Ashtar University, it oversees activity (a.k.a. METFAZ) linked to the Possible Military Dimensions of Iran's nuclear programme upon which Iran is not cooperating with the IAEA.

93. Saman Nasb Zayendeh Unit 7, 3rd Floor Mehdi Building, Construction contractor that has installed 1.12.2011 Rood; Saman Kahorz Blvd, Esfahan, Iran. piping and associated support equipment Nasbzainde Rood at the uranium enrichment site at Natanz. It has dealt specifically with centrifuge piping.

94. Saman Tose'e Asia Engineering firm involved in supporting a 1.12.2011 (SATA) range of large scale industrial projects including Iran's uranium enrichment programme, including undeclared work at the uranium enrichment site at Qom/ Fordow.

95. Samen Industries 2nd km of Khalaj Road End of Shell name for Khorasan Mettalurgy 1.12.2011 Seyyedi St., P.O.Box 91735-549, Industries (designated under UNSCR 91735 Mashhad, Iran, 1803 (2008), subsidiary of Ammunition Tel.: +98 511 3853008, Industries Group (AMIG)) +98 511 3870225

▼M8 _____

▼B

97. STEP Standart Teknik 79/2 Tuzla, 34940, Istanbul, Company run by Milad Jafari, who has 1.12.2011 Parca San ve TIC A.S. Turkey supplied goods, mostly metals, to UN designated Shahid Hemmat Industrial Group (SHIG) through front companies. 02012R0267 — EN — 18.01.2017 — 022.003 — 286

▼B

Name Identifying information Reasons Date of listing

98. SURENA (a.k.a. Company for Construction and Commis 1.12.2011 Sakhd Va Rah-An-Da- sioning of Nuclear Power Plants. Zi) Controlled by the UN designated Novin Energy Company.

99. TABA (Iran Cutting 12 Ferdowsi, Avenue Sakhaee, Owned or controlled by EU-sanctioned 1.12.2011 Tools Manufacturing avenue 30 Tir (sud), nr 66 – TESA, Involved in manufacturing company - Taba Tehran equipment and materials which have Towlid Abzar Boreshi direct applications in the Iranian nuclear Iran) programme.

100. Test Tafsir No 11, Tawhid 6 Street, Moj Company produces and has supplied UF6 1.12.2011 Street, Darya Blvd, Shahrak specific containers to the uranium Gharb, Tehran, Iran. enrichment sites at Natanz and Qom/ Fordow.

101. Tosse Silooha (a.k.a. Involved in the Iranian nuclear 1.12.2011 Tosseh Jahad E Silo) programme at the Natanz, Qom and Arak facilities.

102. Yarsanat (a.k.a. Yar No. 101, West Zardosht Street, Procurement company for UN-designated 1.12.2011 Sanat, a.k.a. Yarestan 3rd Floor, 14157 Tehran; No. Kalaye Electric Company. Involved in Vacuumi) 139 Hoveyzeh Street, 15337, purchasing equipment and materials Tehran. which have direct applications in the Iranian nuclear programme. It has attempted the procurement of vacuum products and pressure transducers.

▼M13 _____

▼M25 _____

▼M8

106. Tidewater (a.k.a. Postal address: No 80, Tidewater Owned or controlled by IRGC 23.01.2012 Tidewater Middle East Building, Vozara Street, Next to Co; Faraz Royal Saie Park, Tehran, Iran Qeshm Company LLC)

▼B

107. Turbine Engineering Postal address: Shishesh Mina Used as a front company by designated 23.1.2012 Manufacturing (TEM) Street, Karaj Special Road, Iran Aircraft Industries (IACI) for covert (a.k.a T.E.M. Co.) Tehran, Iran procurement activities.

▼M9 _____

▼B

109. Rosmachin Postal address: Haftom Tir Front company of Sad Export Import 23.1.2012 Square, South Mofte Avenue, Company. Involved in illicit arms Tour Line No; 3/1, Tehran, Iran transfer aboard M/V Monchgorsk. P.O. Box 1584864813 Tehran, Iran

▼M25 _____

▼M4

131. ██████ ██████ ██████ ██████ ██████ ████ ██████ ██████ ██████ 02012R0267 — EN — 18.01.2017 — 022.003 — 287

▼B

Name Identifying information Reasons Date of listing

▼M25 _____

▼M8

148. Iran Composites Iran Composites Institute, Iranian Composites Institute (ICI, aka 22.12.2012 Institute Iranian University of Science and Composite Institute of Iran) is assisting Technology, designated entities to violate the 16845-188, Tehran, Iran, provisions of UN and EU sanctions on Telephone: 98 217 3912858 Iran and is directly supporting Iran's proliferation sensitive nuclear activities. Fax: 98 217 7491206 As of 2011 ICI had been contracted to E-mail: [email protected] provide EU-designated Iran Centrifuge Website: Technology Company (TESA) with IR- http://www.irancomposites.org 2M centrifuge rotors.

149. Jelvesazan Company 22 Bahman St., Bozorgmehr Ave, Jelvesazan Company is assisting 22.12.2012 84155666, Esfahan, Iran designated entities to violate the Tel: 98 0311 2658311 15 provisions of UN and EU sanctions on Fax: 98 0311 2679097 Iran and is directly supporting Iran's proliferation sensitive nuclear activities. As of early 2012 Jelvesazan intended to supply controlled vacuum pumps to EU- designated Iran Centrifuge Technology Company (TESA).

150. ██████ ██████ ██████ ██████ ██████ ██████ ██████

151. Simatec Development Simatec Development Company is 22.12.2012 Company assisting designated entities to violate the provisions of UN and EU sanctions on Iran and is directly supporting Iran's proliferation sensitive nuclear activities. As of early 2010 Simatec was contracted by UN-designated Kalaye Electric Company (KEC) to procure Vacon inverters to power uranium enrichment centrifuges. As of mid-2012 Simatec was attempting to procure EU-controlled inverters. 02012R0267 — EN — 18.01.2017 — 022.003 — 288

▼M8

Name Identifying information Reasons Date of listing

th 152. Aluminat 1. Parcham St, 13 Km of Qom Aluminat is assisting designated entities 22.12.2012 Rd 38135 Arak (Factory) to violate the provisions of UN and EU th 2. Unit 38, 5 Fl, Bldg No 60, sanctions on Iran and is directly Golfam St, Jordan, 19395- supporting Iran's proliferation sensitive 5716, Tehran nuclear activities. In early 2012 Tel: 98 212 2049216 / Aluminat had a contract to supply 6061- 22049928 / 22045237 T6 aluminium to EU-designated Iran Fax: 98 21 22057127 Centrifuge Technology Company (TESA). Website: www.aluminat.com

153. Organisation of The Organisation of Defensive Innovation 22.12.2012 Defensive Innovation and Research (SPND) is assisting and Research designated persons and entities to violate the provisions of UN and EU sanctions on Iran and is directly supporting Iran's proliferation sensitive nuclear activities. The IAEA has identified SPND with their concerns over possible military dimensions (PMD) to Iran's nuclear programme over which Iran continues to refuse to co-operate. SPND is run by UN- designated Mohsen Fakhrizadeh and is part of the Ministry of Defence For Armed Forces Logistics (MODAFL, designated by the EU in May 2011). Davoud Babaei was designated by the EU in December 2011 in his role as SPND's head of security, in which he is responsible for preventing the disclosure of information including to the IAEA.

▼M25 _____

▼M31 _____

▼M21 _____

▼M17

161. Sharif University of Azadi Ave/Street, PO Box 11365- Sharif University of Technology (SUT) 8.11.2014 Technology 11155, Tehran, Iran, Tel: +98 21 has a number of cooperation agreements 66 161 with Iranian Government organisations which are designated by the UN and/or Email: [email protected] the EU and which operate in military or military-related fields, particularly in the field of ballistic missile production and procurement. This includes: an agreement with the EU-designated Aerospace Industries Organisation for inter alia the production of satellites; cooperating with the Iranian Ministry of Defence and the Iranian Revolutionary Guards Corps (IRGC) on smart boat competitions; a broader agreement with the IRGC Air Force which covers developing and strengthening the Univer sity's relations, organisational and strategic cooperation; 02012R0267 — EN — 18.01.2017 — 022.003 — 289

▼M17

Name Identifying information Reasons Date of listing

SUT is part of a 6-university agreement which supports the Government of Iran through defence-related research; and SUT teaches graduate courses in unmanned aerial vehicle (UAV) engineering which were designed by the Ministry of Science among others. Taken together, these show a significant record of engagement with the Government of Iran in military or military-related fields that constitutes support to the Government of Iran.

▼M8

162. ██████ ██████ ██████ ██████ ██████ ██████ ██████ ██████

▼M25 _____

▼M9

165. ██████ ██████ ██████ ██████ ██████ ██████ ██████

166. ██████ ██████ ██████ ██████ ██████ ██████ ██████

▼M25 _____

▼M29 (1 ) In accordance with Council Implementing Regulation (EU) 2016/603, this entry shall apply until 22 October 2016.

▼B II. ►C1 Iranian Revolutionary Guard Corps (IRGC) ◄

A. Persons

Name Identifying information Reasons Date of listing

1. IRGC Brigadier-General MODAFL Deputy for Inspection. 23.6.2008 Javad DARVISH-VAND Responsible for all MODAFL facilities and installations

2. Rear Admiral Ali Commander of IRGC Navy 26.7.2010 FADAVI 02012R0267 — EN — 18.01.2017 — 022.003 — 290

▼B

Name Identifying information Reasons Date of listing

3. Parviz FATAH born 1961 Khatam al Anbiya's number two 26.7.2010

4. IRGC Brigadier-General Managing Director of the Defence 23.6.2008 Seyyed Mahdi FARAHI Industries Organisation (DIO) which is designated under UNSCR 1737 (2006)

5. IRGC Brigadier-General Head of the General Department of the 23.6.2008 Ali HOSEYNITASH Supreme National Security Council and involved in formulating policy on the nuclear issue

6. IRGC Mohammad Ali Commander of the IRGC 23.6.2008 JAFARI

7. IRGC Brigadier-General Minister for the Interior and former 23.6.2008 Mostafa Mohammad Minister of MODAFL, responsible for NAJJAR all military programmes, including ballistic missiles programmes.

8. BrigGen Mohammad Born in 1953, Nadjaf (Iraq) Commander of Basij Resistance Force 26.7.2010 Reza NAQDI

9. BrigGen Mohammad Commander of IRGC Ground Forces 26.7.2010 PAKPUR

10. Rostam QASEMI (a.k.a. Born in 1961 Commander of Khatam al-Anbiya 26.7.2010 Rostam GHASEMI)

11. BrigGen Hossein Deputy Commander of the IRGC 26.7.2010 SALAMI

12. IRGC Brigadier-General MODAFL Deputy for Counter-Intelli 23.6.2008 Ali SHAMSHIRI gence, responsible for security of MODAFL personnel and Installations

13. IRGC Brigadier-General Minister of the MODAFL and former 23.6.2008 Ahmad VAHIDI Deputy Head of MODAFL

▼M3 _____

▼B

15. Abolghassem Mozaffari Head of Khatam Al-Anbia Construction 1.12.2011 SHAMS Headquarters

▼M3 _____

▼B

17. Ali Ashraf NOURI IRGC Deputy Commander, IRGC 23.1.2012 Political Bureau Chief

18. Hojatoleslam Ali SAIDI Representative of the Supreme Leader to 23.1.2012 (a.k.a. Hojjat- al-Eslam the IRGC Ali Saidi or Saeedi

19. Amir Ali Haji ZADEH IRGC Air Force Commander, Brigadier 23.1.2012 (a.k.a. Amir Ali General Hajizadeh) 02012R0267 — EN — 18.01.2017 — 022.003 — 291

▼B

B. Entities

Name Identifying information Reasons Date of listing

1. ►C1 Iranian Revolu- Tehran, Iran Responsible for Iran's nuclear 26.7.2010 tionary Guard Corps ◄ programme. Has operational control for (IRGC) Iran's ballistic missile programme. Has undertaken procurement attempts to support Iran's ballistic missiles and nuclear programmes

2. IRGC Air Force Operates Iran's inventory of short and 23.6.2008 medium range ballistic missiles. The head of the IRGC air force was designated by UNSCR 1737 (2006)

3. IRGC-Air Force Al- The IRGC-Air Force Al-Ghadir Missile 26.7.2010 Ghadir Missile Command is a specific element within Command the IRGC Air Force that has been working with SBIG (designated under UNSCR 1737) with the FATEH 110, short range ballistic missile as well as the Ashura medium range ballistic missile. This command appears to be the entity that actually has the operational control of the missiles.

4. Naserin Vahid Naserin Vahid produces weapons parts 26.7.2010 on behalf of the IRGC. An IRGC front company.

5. IRGC Qods Force Tehran, Iran Iran's ►C1 Iranian Revolutionary 26.7.2010 Guard Corps ◄ (IRGC) Qods Force is responsible for operations outside Iran and is Tehran's principal foreign policy tool for special operations and support to terrorists and Islamic militants abroad. Hizballah used Qods Force- supplied rockets, anti-ship cruise missiles (ASCMs), man-portable air defense systems (MANPADS), and unmanned aerial vehicles (UAVs) in the 2006 conflict with Israel and benefited from Qods Force training on these systems, according to press reporting. According to a varietyof reports, the Qods Force continues to re-supply and train Hizballah on advanced weaponry, anti-aircraft missiles, and long-range rockets. The Qods Force continues to provide limited lethal support, training, and funding to Taliban fighters in southern and western Afghanistan including small arms, ammunition, mortars, and short- range battlefield rockets. Commander has been sanctioned under UNSCR 02012R0267 — EN — 18.01.2017 — 022.003 — 292

▼B

Name Identifying information Reasons Date of listing

6. Sepanir Oil and Gas A subsidiary of Khatam al-Anbya 26.7.2010 Energy Engineering Construction Headquarters which was Company (a.k.a. Sepah designated under UNSCR 1929. Nir) Sepanir Oil and Gas Engineering Company is participating in Iran's South Pars offshore Phase 15-16 gas field development project.

7. Bonyad Taavon Sepah Niayes Highway, Seoul Street, Bonyad Taavon Sepah, also known as 23.05.2011 (a.k.a. IRGC Tehran, Iran the IRGC Cooperative Foundation, was Cooperative Foundation; formed by the Commanders of the Bonyad-e Ta'avon- IRGC to structure the IRGC's invest Sepah; Sepah ments. It is controlled by the IRGC. Cooperative Foundation) Bonyad Taavon Sepah's Board of Trustees is composed of nine members, of whom eight are IRGC members. These officers include the IRGC's Commander in Chief, who is the Chairman of the Board of Trustees, the Supreme Leader's representative to the IRGC, the Basij commander, the IRGC Ground Forces commander, the IRGC Air Force commander, the IRGC Navy commander, the head of the IRGC Information Security Organization, a senior IRGC officer from the Armed Forces General Staff, and a senior IRGC officer from MODAFL.

8. Ansar Bank (a.k.a. Ansar No. 539, North Pasdaran Avenue, Bonyad Taavon Sepah created Ansar 23.05.2011 Finance and Credit Tehran; Ansar Building, North Bank to provide financial and credit Fund; Ansar Financial Khaje Nasir Street, Tehran, Iran services to IRGC personnel. Initially, and Credit Institute; Ansar Bank operated as a credit union Ansae Institute; Ansar and transitioned in to a fully fledged al-Mojahedin No-Interest bank in mid 2009, upon receiving a Loan Institute; Ansar licence from Iran's Central bank. Ansar Saving and Interest Free- Bank, formerly known as Ansar al Loans Fund) Mojahedin, has been linked to the IRGC for over 20 years. IRGC members received their salaries through Ansar bank. In addition, Ansar bank provided special benefits to IRGC personnel, includingreduced rates for home furnishings and free, or reduced- cost, health care.

9. Mehr Bank (a.k.a Mehr 204 Taleghani Ave., Tehran, Iran Mehr Bank is controlled by Bonyas 23.05.2011 Finance and Credit Taavon Sepah and the IRGC. Mehr Institute; Mehr Interest- Bank provides financial services to the Free Bank) IRGC. According to an open source interview with the head of Bonyad Taavon Sepah, Parviz Fattah (b. 1961), Bonyad Taavon Sepah created Mehr Bank to serve the Basij (paramilitary arm of the IRGC). 02012R0267 — EN — 18.01.2017 — 022.003 — 293

▼B

Name Identifying information Reasons Date of listing

▼M9 _____

▼B

11. Behnam Sahriyari Postal address: Ziba Buidling, 10th Sent two containers of various types of 23.1.2012 Trading Company Floor, Northern Sohrevardi Street, firearms from Iran to Syria in May 2007 Tehran, Iran in violation of op. 5 of UNSCR 1747(2007)

III. Islamic Republic of Iran Shipping Lines (IRISL)

A. Person

Name Identifying information Reasons Date of listing ▼M25 _____

▼B

2. ██████ ██████████████████ ██████ ██████

3. ██████ ██████████████████ ██████ ██████

4. ██████ ██████████████████ ██████ ██████

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▼M9

6. ██████ █████████████ ██████ ██████ ████████████ █████████████ 02012R0267 — EN — 18.01.2017 — 022.003 — 294

▼B

Name Identifying information Reasons Date of listing

7. ██████ ██████ ██████

▼M25 _____

▼B

9. ██████ ██████████████████ ██████ ██████

10. ██████ ██████████████████ ██████ ██████

▼M9

11. ██████ ██████████████████ ██████ ██████

▼B

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13. ██████ ████████████ ██████ ██████ ██████ ████████████ ████████████ 02012R0267 — EN — 18.01.2017 — 022.003 — 295

▼B

Name Identifying information Reasons Date of listing

▼M12

14. ██████ ██████████████████ ██████ ██████

▼B B. Entities

Name Identifying information Reasons Date of listing

1. ██████ ██████████████ ██████ ██████ ██████ ██████

██ ██████ ██████████████ ██████ ██████ ██████

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██ ██████ ██████ ██████ ██████

k) IRITAL Shipping Commercial Registry Number: GE Point of contact for ECL and PCL 26.7.2010 SRL 426505 (Italy); Italian Fiscal Code: services. Used by the DIO subsidiary 03329300101 (Italy); V.A.T. Marine Industries Group (MIG; now Number: 12869140157 (Italy) known as Marine Industries Ponte Francesco Morosini 59, Organization, MIO) which is 16126 Genova (GE), Italy; responsible for the design and construction of various marine structures and both military and non- military vessels. DIO was designated under UNSCR 1737.

██ ██████ ██████ ██████ ██████ ██████

██ ██████ ████████████ ██████ ██████

██ ██████ ██████ ██████ ██████ 02012R0267 — EN — 18.01.2017 — 022.003 — 296

▼B

Name Identifying information Reasons Date of listing

██ ██████ ██████ ██████ ██████

██ ██████ ██████ ██████ ██████ ██████ ██████ ██████

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▼M25 _____

▼B

25. ██████ ████████████ ██████ ██████ ██████

26. ██████ ███████ ██████ ██████ ██████

26.a. ██████ ██████ ██████ ██████ ██████

26.b. ██████ ██████ ██████ ██████ ██████

26.c. ██████ ██████ ██████ ██████ ██████

26.d. ██████ ██████ ██████ ██████ ██████

27. ██████ ███████ ██████ ██████ ██████ ██████ 02012R0267 — EN — 18.01.2017 — 022.003 — 297

▼B

Name Identifying information Reasons Date of listing

▼M25 _____

▼M4 _____

▼M25 _____

▼M9

43. ██████ ██████ ██████ ██████ ██████ ██████ ██████

▼M25 _____

▼M4 _____

▼M25 _____

▼M1 _____

▼M25 _____

▼M21 _____

▼M8 _____

▼M25 _____

▼M21 _____

▼M25 _____

▼M9 _____ 02012R0267 — EN — 18.01.2017 — 022.003 — 298

▼B

Name Identifying information Reasons Date of listing ▼M25 _____

▼M21 _____

▼M25 _____

▼M1 _____

▼M25 _____

▼M21 _____

▼M25 _____

▼M21 _____

▼M25 _____

▼M12

154. ██████ █████████████ ██████ ██████ █████████████ ▼M25 _____ 02012R0267 — EN — 18.01.2017 — 022.003 — 299

▼M24 ANNEX X

Websites for information on the competent authorities and address for notification to the European Commission

BELGIUM http://www.diplomatie.be/eusanctions

BULGARIA http://www.mfa.bg/en/pages/135/index.html

CZECH REPUBLIC http://www.mfcr.cz/mezinarodnisankce

DENMARK http://um.dk/da/politik-og-diplomati/retsorden/sanktioner/

GERMANY http://www.bmwi.de/DE/Themen/Aussenwirtschaft/ aussenwirtschaftsrecht,did=404888.html

ESTONIA http://www.vm.ee/est/kat_622/

IRELAND http://www.dfa.ie/home/index.aspx?id=28519

GREECE http://www.mfa.gr/en/foreign-policy/global-issues/international-sanctions.html

SPAIN http://www.exteriores.gob.es/Portal/es/PoliticaExteriorCooperacion/ GlobalizacionOportunidadesRiesgos/Documents/ORGANISMOS% 20COMPETENTES%20SANCIONES%20INTERNACIONALES.pdf

FRANCE http://www.diplomatie.gouv.fr/autorites-sanctions/

CROATIA http://www.mvep.hr/sankcije

ITALY http://www.esteri.it/MAE/IT/Politica_Europea/Deroghe.htm

CYPRUS http://www.mfa.gov.cy/sanctions

LATVIA http://www.mfa.gov.lv/en/security/4539

LITHUANIA http://www.urm.lt/sanctions

LUXEMBOURG http://www.mae.lu/sanctions

HUNGARY http://2010-2014.kormany.hu/download/b/3b/ 70000/ENSZBT-ET-szankcios-tajekoztato.pdf 02012R0267 — EN — 18.01.2017 — 022.003 — 300

▼M24 MALTA https://www.gov.mt/en/Government/Government%20of%20Malta/ Ministries%20and%20Entities/Officially%20Appointed%20Bodies/Pages/Boards/ Sanctions-Monitoring-Board-.aspx NETHERLANDS http://www.rijksoverheid.nl/onderwerpen/internationale-sancties AUSTRIA http://www.bmeia.gv.at/view.php3?f_id=12750&LNG=en&version= POLAND http://www.msz.gov.pl PORTUGAL http://www.portugal.gov.pt/pt/os-ministerios/ministerio-dos-negocios-estrangeiros/ quero-saber-mais/sobre-o-ministerio/medidas-restritivas/medidas-restritivas.aspx ROMANIA http://www.mae.ro/node/1548 SLOVENIA http://www.mzz.gov.si/si/omejevalni_ukrepi SLOVAKIA http://www.mzv.sk/sk/europske_zalezitosti/europske_politiky-sankcie_eu FINLAND http://formin.finland.fi/kvyhteistyo/pakotteet SWEDEN http://www.ud.se/sanktioner UNITED KINGDOM https://www.gov.uk/sanctions-embargoes-and-restrictions Address for notifications to the European Commission: European Commission Service for Foreign Policy Instruments (FPI) EEAS 02/309 B-1049 Brussels Belgium E-mail: [email protected]

______02012R0267 — EN — 18.01.2017 — 022.003 — 301

▼M24 ANNEX XIII

List of persons, entities and bodies referred to in Article 23a(1)

A. Natural persons B. Entities and bodies 02012R0267 — EN — 18.01.2017 — 022.003 — 302

▼M24 ANNEX XIV

List of persons, entities and bodies referred to in Article 23a(2)

A. Natural persons B. Entities and bodies