ANNEX III Restricted Nuclear Goods, Commodities, and Technologies
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A Guide to Export Controls
Foreign Affairs, Trade and Affaires étrangères, Commerce et Development Canada Développment Canada A Guide To CANADA’S EXPORT CONTROLS December 2012 Introduction The issuance of export permits is administered by the Export Controls Division (TIE) of Foreign Affairs, Trade and Development Canada (DFATD). TIE provides assistance to exporters in determining if export permits are required. It also publishes brochures and Notices to Exporters that are freely available on request and on our website www.exportcontrols.gc.ca. How to contact us: Export Controls Division (TIE) Foreign Affairs, Trade and Development Canada 111 Sussex Drive Ottawa, Ontario K1A 0G2 Telephone: (613) 996-2387 Facsimile: (613) 996-9933 Email: [email protected] For information on how to apply for an export permit and additional information on export controls please refer to our website. To enquire on the status of an export permit application: Recognized EXCOL users can check the status of an export permit application on-line. Non-recognized users can call (613) 996-2387 or email [email protected] and quote your export permit application identification (ref ID) number. Export Controls Division website: www.exportcontrols.gc.ca This Guide, at time of publication, encompasses the list of items enumerated on the Export Control List (ECL) that are controlled for export in accordance with Canadian foreign policy, including Canada’s participation in multilateral export control regimes and bilateral agreements. Unless otherwise specified, the export controls contained in this Guide apply to all destinations except the United States. Canada’s Export Control List can be found at the Department of Justice website at http://canada.justice.gc.ca/. -
High-Strength Aluminum P/M Alloys
ASM Handbook, Volume 2: Properties and Selection: Nonferrous Alloys and Special-Purpose Materials Copyright © 1990 ASM International® ASM Handbook Committee, p 200-215 All rights reserved. DOI: 10.1361/asmhba0001064 www.asminternational.org High-Strength Aluminum P/M Alloys J.R. Pickens, Martin Marietta Laboratories POWDER METALLURGY (P/M) tech- one of the dominant structural material fam- of particular concern to designers of aircraft nology provides a useful means of fabricating ilies of the 20th century. Aluminum has low and aerospace structures, where high ser- net-shape components that enables machin- density (2.71 g/cm 3) compared with compet- vice temperatures preclude the use of alu- ing to be minimized, thereby reducing costs. itive metallic alloy systems, good inherent minum alloys for certain structural compo- Aluminum P/M alloys can therefore compete corrosion resistance because of the contin- nents. with conventional aluminum casting alloys, uous, protective oxide film that forms very The number of alloying elements that as well as with other materials, for cost- quickly in air, and good workability that have extensive solid solubility in aluminum critical applications. In addition, P/M technol- enables aluminum and its alloys to be eco- is relatively low. Consequently, there are ogy can be used to refine microstructures nomically rolled, extruded, or forged into not many precipitation-hardenable alumi- compared with those made by conventional useful shapes. Major alloying additions to num alloy systems that are practical by ingot metallurgy (I/M), which often results in aluminum such as copper, magnesium, conventional I/M. This can be viewed as a improved mechanical and corrosion proper- zinc, and lithium--alone, or in various limitation when alloy developers endeavor ties. -
WO 2016/074683 Al 19 May 2016 (19.05.2016) W P O P C T
(12) INTERNATIONAL APPLICATION PUBLISHED UNDER THE PATENT COOPERATION TREATY (PCT) (19) World Intellectual Property Organization International Bureau (10) International Publication Number (43) International Publication Date WO 2016/074683 Al 19 May 2016 (19.05.2016) W P O P C T (51) International Patent Classification: (81) Designated States (unless otherwise indicated, for every C12N 15/10 (2006.01) kind of national protection available): AE, AG, AL, AM, AO, AT, AU, AZ, BA, BB, BG, BH, BN, BR, BW, BY, (21) International Application Number: BZ, CA, CH, CL, CN, CO, CR, CU, CZ, DE, DK, DM, PCT/DK20 15/050343 DO, DZ, EC, EE, EG, ES, FI, GB, GD, GE, GH, GM, GT, (22) International Filing Date: HN, HR, HU, ID, IL, IN, IR, IS, JP, KE, KG, KN, KP, KR, 11 November 2015 ( 11. 1 1.2015) KZ, LA, LC, LK, LR, LS, LU, LY, MA, MD, ME, MG, MK, MN, MW, MX, MY, MZ, NA, NG, NI, NO, NZ, OM, (25) Filing Language: English PA, PE, PG, PH, PL, PT, QA, RO, RS, RU, RW, SA, SC, (26) Publication Language: English SD, SE, SG, SK, SL, SM, ST, SV, SY, TH, TJ, TM, TN, TR, TT, TZ, UA, UG, US, UZ, VC, VN, ZA, ZM, ZW. (30) Priority Data: PA 2014 00655 11 November 2014 ( 11. 1 1.2014) DK (84) Designated States (unless otherwise indicated, for every 62/077,933 11 November 2014 ( 11. 11.2014) US kind of regional protection available): ARIPO (BW, GH, 62/202,3 18 7 August 2015 (07.08.2015) US GM, KE, LR, LS, MW, MZ, NA, RW, SD, SL, ST, SZ, TZ, UG, ZM, ZW), Eurasian (AM, AZ, BY, KG, KZ, RU, (71) Applicant: LUNDORF PEDERSEN MATERIALS APS TJ, TM), European (AL, AT, BE, BG, CH, CY, CZ, DE, [DK/DK]; Nordvej 16 B, Himmelev, DK-4000 Roskilde DK, EE, ES, FI, FR, GB, GR, HR, HU, IE, IS, IT, LT, LU, (DK). -
Reinforcements—The Key to High Performance Composite Materials
^_ a ^-9I NASA Technical Memorandum 103230 Reinforcements—The Key to High Performance Composite Materials Salvatore J. Grisaffe Lewis Research Center Cleveland, Ohio Prepared for the Complex Composites Workshop sponsored by the Japanese Technology Evaluation Center Washington, DC, March 27, 1990 NASA REINFORCEMENTS - THE KEY TO HIGH-PERFORMANCE COMPOSITE MATERIALS Salvatore J. Grisaffe National Aeronautics and Space Administration Lewis Research Center Cleveland, Ohio 44135 INTRODUCTION High-temperature reinforcements are the key to high-performance composite materials. Such materials are the critical enabling technological issue in the design and development of 21st-century aerospace propulsion and power systems. The purpose of this section is to review some of the insights and findings developed on Japanese fibers and whiskers during the Japanese Technology Evalu- ation Center (JTEC) one-week visit to Japan and to examine these in light of current U.S. fiber technology. Conventional materials are too heavy to provide effective structural mem- bers for future flight systems. The estimated cost of moving 1 pound to orbit is about $1000; cost per pound to the Noon is about $50,000; and cost per pound to Mars is about $500,000. Thus, the payoff for low-density, high-strength fibers and composites becomes clear. Figure 1 shows how high-performance com- posites could generally benefit any future high-speed civil transport aircraft. NOx intrusion and noise must be overcome before such an aircraft can be consid- ered feasible. Minimal environmental intrusion is contingent on combustors that can operate at extremely high temperatures and so , must ,be constructed of, for example, ceramic matrix composites. -
Applications of an Aluminum-Beryllium Composite for Structural Aerospace Components
Applications of an Aluminum -Beryllium Composite for Structural Aerospace Components William Speer and Omar S. Es -Said Mechanical Engineering Department, Loyola Marymount University, 7900 Loyola Blvd, Los Angeles, CA 90045 -8145, USA Abstract The us e of AlBeMet AM162, an aluminum -beryllium metal matrix composite, is an effective way to reduce the size and weight of many structural aerospace components that are currently made out of aluminum and titanium alloys. These savings, which are essential for today’s technologies, are primarily due to the material’s high modulus and low density combined with its better than average specific strength. The raw material costs are significantly higher than they are for traditional engineering alloys, and the avai lable billet sizes are more limited than they are for aluminum and titanium alloys. Although the material costs are higher for the aluminum -beryllium composite, ease of machining makes it financially competitive when compared to equivalent parts made out of titanium alloys. Due to toxic nature of beryllium, however, debris -generating operations must be strictly regulated to limit worker’s exposure to the material and protect them from potentially fatal diseases. Keywords: Metal matrix; AlBeMet; High el astic modulus; Low density; Weight reduction; Stiffness -driven design 1. Introduction The aerospace industry is continually searching for ways to reduce the weight of its products and maximize the amount of profit -making payload in launch vehicles. One o f the most common ways engineers reduce weight is to make their products out of low-density alloys or engineering composites. These materials offer very high strength and/or stiffness to weight ratios; therefore, they require less mass and take less space to support a given load in comparison to other material choices. -
Controls the Level of Power in the Core, and the Components Which Normally Contain, Come Into Direct Contact with Or Control the Primary Coolant of the Reactor Core;
Document Generated: 2019-11-16 Status: This is the original version (as it was originally made). This item of legislation is currently only available in its original format. SCHEDULE 1 PROHIBITED GOODS PART III GROUP 2 ATOMIC ENERGY MINERALS AND MATERIALS AND NUCLEAR FACILITIES, EQUIPMENT, APPLIANCES AND SOFTWARE Interpretations and definitions In this Group: “boron equivalent” (BE) is defined as: BE = CF × Concentration of element Z in ppm and gammaB and gammaZ are the thermal neutron capture cross sections (in barns) for boron and element Z respectively; and AB and AZ are the atomic weights of boron and element Z respectively; “depleted uranium” means uranium depleted in the isotope 235 below that occurring in nature; “effective gramme” of special fissile material or other fissile material means: a. for plutonium isotopes and uranium-233, the isotope weight in grammes; b. for uranium enriched 1 per cent or greater in the isotope U-235, the element weight in grammes multiplied by the square of its enrichment expressed as a decimal weight fraction; c. for uranium enriched below 1 per cent in the isotope U-235, the element weight in grammes multiplied by 0.0001; d. for americium-242m, curium-245 and curium-247, californium-249 and californium-251, the isotope weight in grammes multiplied by 10; “fibrous or filamentary materials” include: a. continuous monofilaments; b. continuous yarns and rovings; c. tapes, fabrics, random mats and braids; d. chopped fibres, staple fibres and coherent fibre blankets; e. whiskers, either monocrystalline -
A Review of Metastable Beta Titanium Alloys
metals Review A Review of Metastable Beta Titanium Alloys R. Prakash Kolli 1,* ID and Arun Devaraj 2 1 Department of Materials Science and Engineering, University of Maryland, College Park, MD 20742, USA 2 Physical and Computational Sciences Directorate, Pacific Northwest National Laboratory, Richland, WA 99354, USA; [email protected] * Correspondence: [email protected]; Tel.: +1-301-405-5217; Fax: 301-405-6327 Received: 21 May 2018; Accepted: 25 June 2018; Published: 30 June 2018 Abstract: In this article, we provide a broad and extensive review of beta titanium alloys. Beta titanium alloys are an important class of alloys that have found use in demanding applications such as aircraft structures and engines, and orthopedic and orthodontic implants. Their high strength, good corrosion resistance, excellent biocompatibility, and ease of fabrication provide significant advantages compared to other high performance alloys. The body-centered cubic (bcc) b-phase is metastable at temperatures below the beta transus temperature, providing these alloys with a wide range of microstructures and mechanical properties through processing and heat treatment. One attribute important for biomedical applications is the ability to adjust the modulus of elasticity through alloying and altering phase volume fractions. Furthermore, since these alloys are metastable, they experience stress-induced transformations in response to deformation. The attributes of these alloys make them the subject of many recent studies. In addition, researchers are pursuing development of new metastable and near-beta Ti alloys for advanced applications. In this article, we review several important topics of these alloys including phase stability, development history, thermo-mechanical processing and heat treatment, and stress-induced transformations. -
L 340 Official Journal
Official Journal L 340 of the European Union Volume 58 English edition Legislation 24 December 2015 Contents II Non-legislative acts REGULATIONS ★ Commission Delegated Regulation (EU) 2015/2420 of 12 October 2015 amending Council Regulation (EC) No 428/2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual use items . 1 Acts whose titles are printed in light type are those relating to day-to-day management of agricultural matters, and are generally valid for a limited period. The titles of all other acts are printed in bold type and preceded by an asterisk. EN 24.12.2015 EN Official Journal of the European Union L 340/1 II (Non-legislative acts) REGULATIONS COMMISSION DELEGATED REGULATION (EU) 2015/2420 of 12 October 2015 amending Council Regulation (EC) No 428/2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual use items THE EUROPEAN COMMISSION, Having regard to the Treaty on the Functioning of the European Union, Having regard to Council Regulation (EC) No 428/2009 of 5 May 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual use items ( 1 ) and in particular Article 15(3) thereof, Whereas: (1) Regulation (EC) No 428/2009 requires dual-use items to be subject to effective control when they are exported from or transit through the Union, or are delivered to a third country as a result of brokering services provided by a broker resident or established in the Union. (2) Annex I to Regulation (EC) No 428/2009 establishes the common list of dual-use items that are subject to controls in the Union. -
FINANCIAL INTELLIGENCE CENTRE (FIC) Circular No.22 of 2014
FINANCIAL INTELLIGENCE CENTRE (FIC) Circular No.22 of 2014 Additional obligations for Accountable Institutions (AIs) and Reporting Institutions (RIs) to report Suspicious Transactions(STRs) and Suspicious Activities(SARs) relating to Financing of Terrorism (FT) and Proliferation (PF), section 33 of the Financial Intelligence Act 2012, Act 13 of 2012, as amended (herein referred to as The FIA). Introduction This circular is issued in terms of Section 9(1) (h) of The FIA and bears reference to the issued Financial Intelligence Centre (FIC) Circular 1 of 2013. The FIC, as part of its continued efforts to assist the Government of the Republic of Namibia to reduce the National Money Laundering (ML), Terrorist Financing (TF) and Proliferation Financing (PF) risks will be circulating lists derived from the United Nations Security Council of designated individuals, entities and other groups1. These lists will be communicated via circulars to AIs and RIs whenever updates are made on the said lists. The United Nations Security Council Resolution lists (1267, 1988, 1718 & 1737) Attached hereto find the following UN Security Council lists on which Accountable Institutions (AIs) and Reporting Institutions (RIs) are required to take relevant action as per the FIA: 1. Annexure “A” The List established and maintained by the 1267 Committee with respect to individuals, groups, undertakings and other entities associated with Al- Qaida as updated on 23 September 2014. The Al-Qaida Sanctions List consists of two sections, specified below: a) Individuals associated with Al-Qaida: and b) Entities and other groups and undertakings associated with Al- Qaida. 1 This is as per mandated by the Prevention and Combatting of Terrorist and Proliferation Activities Act, 2014 (Act No. -
Chapter 16 Composites
1496T_c16_577-620 12/31/05 14:08 Page 577 2nd REVISE PAGES Chapter 16 Composites Top. ABS plastic having Bidirectional layers. 45 a low glass transition temperature. fiberglass. Provide torsional Used for containment and cosmetic stiffness. purposes. Unidirectional layers. 0 (and Side. ABS plastic some 90 ) fiberglass. Provide having a low glass longitudinal stiffness. transition temperature. Containment and cosmetic. Core wrap. Bidirectional layer of fiberglass. Acts as a torsion box and bonds outer layers to core. Core. Polyurethane plastic. Acts as a filler. Bidirectional layer. 45 fiberglass. Damping layer. Polyurethane. Provides torsional Improves chatter resistance. stiffness. Unidirectional layers. 0 (and some 90 ) fiberglass. Provide longitudinal stiffness. Edge. Hardened steel. Facilitates Bidirectional layer. 45 fiberglass. turning by “cutting” Provides torsional stiffness. into the snow. Base. Compressed carbon (carbon particles embedded in a plastic matrix). Hard and abrasion resistant. Provides appropriate surface. One relatively complex composite structure is the modern ski. In this illustration, a cross section of a high-performance snow ski, are shown the various components. The function of each component is noted, as well as the material that is used in its construction. (Courtesy of Evolution Ski Company, Salt Lake City, Utah.) WHY STUDY Composites? With a knowledge of the various types of composites, property combinations that are better than those as well as an understanding of the dependence of found in the metal alloys, ceramics, and polymeric their behaviors on the characteristics, relative amounts, materials. For example, in Design Example 16.1, we geometry/distribution, and properties of the con- discuss how a tubular shaft is designed that meets stituent phases, it is possible to design materials with specified stiffness requirements. -
Security Council Distr.: General 28 November 2001
U nited N ations S /2001/1120 Security Council Distr.: General 28 November 2001 Original: English Letter dated 27 November 2001 from the Deputy Permanent Representative of the United States of America to the United Nations addressed to the President of the Security Council I have the honour to draw your attention to the dual-use list issued on 27 November 2001 (see annex). I should be grateful if you would have the text of this letter and its annex circulated as a document of the Security Council. (Signed) Jam es B. Cunnigham Am bassador 01-66645 (E) 291101 S/2001/1120 Annex to the letter dated 27 Novem ber 2001 from the Deputy Permanent Representative of the United States of America to the United Nations addressed to the President of the Security Council Dual-use goods and technologies Contents Page List of dual-use goods and technologies - General Technology and General Software Notes ...................... 3 - Category 1. Materials............................................. 4 - Category 2. Materials Processing ................................... 20 - Category 3. Electronics ........................................... 39 - Category 4. Computers ........................................... 51 - Category 5. Part 1 Telecom m unications .............................. 62 - Category 5. Part 2 Inform ation Security .............................. 68 - Category 6. Sensors and Lasers ..................................... 72 - Category 7. Navigation and Avionics ................................ 96 -Category 8. Marine............................................. -
Structure and Properties of Titanium Tantalum Alloys for Biocompatibility
Structure and Properties of Titanium Tantalum Alloys for Biocompatibility Dissertation Presented in Partial Fulfillment of the Requirements for the Degree Doctor of Philosophy in the Graduate School of The Ohio State University By Daniel E. Huber Graduate Program in Materials Science and Engineering The Ohio State University 2016 Committee: Dr. Hamish L. Fraser, Advisor Dr. David McComb Dr. Stephen Niezgoda Copyrighted by Daniel E. Huber 2016 Abstract In this thesis, the phase stability and elastic modulus of Ti–Ta simple binary alloys as well as alloys with small additions of ternary elements have been studied. The binary alloy from a nominal 8 to 28 wt.% Ta was first explored using a combinatorial approach. This approach included Laser Engineered Net Shape (LENS™) processing of materials and subsequent characterization by instrumented indentation and site specific Transmission Electron Microscopy (TEM). The composition range of 15 to 75 wt.% Ta was further explored by more traditional methods that included vacuum arc melting high purity elements, X-Ray Diffraction (XRD) and modulus measurements made by ultrasonic methods. Beyond the simple binary, alloys with low levels of ternary elements, oxygen, aluminum, zirconium and small additions of rare earth oxides were investigated. The crystal structure with space group Cmcm was chosen for it applicability with P63/mmc and !"3! sub group / super group symmetry. This provides a consistent crystal structure framework for the purpose of studying the α to β transformation pathway and associated α’ and α’’ martensitic phases. In this case, the pathway is defined by both the lattice parameters and the value of the parameter “y”, where the parameter “y” describes the atomic positions of the [002]α’’ plane.