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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/. -
Of 10 October 2018 Amending Council Regulation (EC) No 428/2009
14.12.2018 EN Official Journal of the European Union L 319/1 II (Non-legislative acts) REGULATIONS COMMISSION DELEGATED REGULATION (EU) 2018/1922 of 10 October 2018 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. Decisions on the items subject to controls are taken within the framework of the Australia Group ( 2 ), the Missile Technology Control Regime ( 3 ), the Nuclear Suppliers Group ( 4 ), the Wassenaar Arrangement ( 5 ) and the Chemical Weapons Convention. (3) The list of dual-use items set out in Annex I to Regulation (EC) No 428/2009 needs to be updated regularly so as to ensure full compliance with international security obligations, to guarantee transparency, and to maintain the competitiveness of economic operators. -
Investigation of Condensed and Early Stage Gas Phase Hypergolic Reactions Jacob Daniel Dennis Purdue University
Purdue University Purdue e-Pubs Open Access Dissertations Theses and Dissertations Fall 2014 Investigation of condensed and early stage gas phase hypergolic reactions Jacob Daniel Dennis Purdue University Follow this and additional works at: https://docs.lib.purdue.edu/open_access_dissertations Part of the Propulsion and Power Commons Recommended Citation Dennis, Jacob Daniel, "Investigation of condensed and early stage gas phase hypergolic reactions" (2014). Open Access Dissertations. 256. https://docs.lib.purdue.edu/open_access_dissertations/256 This document has been made available through Purdue e-Pubs, a service of the Purdue University Libraries. Please contact [email protected] for additional information. i INVESTIGATION OF CONDENSED AND EARLY STAGE GAS PHASE HYPERGOLIC REACTIONS A Dissertation Submitted to the Faculty of Purdue University by Jacob Daniel Dennis In Partial Fulfillment of the Requirements for the Degree of Doctor of Philosophy December 2014 Purdue University West Lafayette, Indiana ii To my parents, Jay and Susan Dennis, who have always pushed me to be the person they know I am capable of being. Also to my wife, Claresta Dennis, who not only tolerated me but suffered along with me throughout graduate school. I love you and am so proud of you! iii ACKNOWLEDGEMENTS I would like to express my sincere gratitude to my advisor, Dr. Timothée Pourpoint, for guiding me over the past four years and helping me become the researcher that I am today. In addition I would like to thank the rest of my PhD Committee for the insight and guidance. I would also like to acknowledge the help provided by my fellow graduate students who spent time with me in the lab: Travis Kubal, Yair Solomon, Robb Janesheski, Jordan Forness, Jonathan Chrzanowski, Jared Willits, and Jason Gabl. -
Rocket Propulsion Fundamentals 2
https://ntrs.nasa.gov/search.jsp?R=20140002716 2019-08-29T14:36:45+00:00Z Liquid Propulsion Systems – Evolution & Advancements Launch Vehicle Propulsion & Systems LPTC Liquid Propulsion Technical Committee Rick Ballard Liquid Engine Systems Lead SLS Liquid Engines Office NASA / MSFC All rights reserved. No part of this publication may be reproduced, distributed, or transmitted, unless for course participation and to a paid course student, in any form or by any means, or stored in a database or retrieval system, without the prior written permission of AIAA and/or course instructor. Contact the American Institute of Aeronautics and Astronautics, Professional Development Program, Suite 500, 1801 Alexander Bell Drive, Reston, VA 20191-4344 Modules 1. Rocket Propulsion Fundamentals 2. LRE Applications 3. Liquid Propellants 4. Engine Power Cycles 5. Engine Components Module 1: Rocket Propulsion TOPICS Fundamentals • Thrust • Specific Impulse • Mixture Ratio • Isp vs. MR • Density vs. Isp • Propellant Mass vs. Volume Warning: Contents deal with math, • Area Ratio physics and thermodynamics. Be afraid…be very afraid… Terms A Area a Acceleration F Force (thrust) g Gravity constant (32.2 ft/sec2) I Impulse m Mass P Pressure Subscripts t Time a Ambient T Temperature c Chamber e Exit V Velocity o Initial state r Reaction ∆ Delta / Difference s Stagnation sp Specific ε Area Ratio t Throat or Total γ Ratio of specific heats Thrust (1/3) Rocket thrust can be explained using Newton’s 2nd and 3rd laws of motion. 2nd Law: a force applied to a body is equal to the mass of the body and its acceleration in the direction of the force. -
Orbital Fueling Architectures Leveraging Commercial Launch Vehicles for More Affordable Human Exploration
ORBITAL FUELING ARCHITECTURES LEVERAGING COMMERCIAL LAUNCH VEHICLES FOR MORE AFFORDABLE HUMAN EXPLORATION by DANIEL J TIFFIN Submitted in partial fulfillment of the requirements for the degree of: Master of Science Department of Mechanical and Aerospace Engineering CASE WESTERN RESERVE UNIVERSITY January, 2020 CASE WESTERN RESERVE UNIVERSITY SCHOOL OF GRADUATE STUDIES We hereby approve the thesis of DANIEL JOSEPH TIFFIN Candidate for the degree of Master of Science*. Committee Chair Paul Barnhart, PhD Committee Member Sunniva Collins, PhD Committee Member Yasuhiro Kamotani, PhD Date of Defense 21 November, 2019 *We also certify that written approval has been obtained for any proprietary material contained therein. 2 Table of Contents List of Tables................................................................................................................... 5 List of Figures ................................................................................................................. 6 List of Abbreviations ....................................................................................................... 8 1. Introduction and Background.................................................................................. 14 1.1 Human Exploration Campaigns ....................................................................... 21 1.1.1. Previous Mars Architectures ..................................................................... 21 1.1.2. Latest Mars Architecture ......................................................................... -
Design, Analysis, and Simulation of Rocket Propulsion System By
Design, Analysis, and Simulation of Rocket Propulsion System By Sarah L. Kulhanek Submitted to the graduate degree program in Aerospace Engineering and the Graduate Faculty of the University of Kansas in partial fulfillment of the requirements for the degree of Masters of Science. ________________________________ Chairperson, Dr. Ray Taghavi ________________________________ Committee member, Dr. Saeed Farokhi ________________________________ Committee member, Dr. Shahriar Keshmiri Date Defended: 6/6/2012 The Thesis Committee for Sarah L. Kulhanek certifies that this is the approved version of the following thesis: Design, Analysis, and Simulation of Rocket Propulsion System __________________________________ Chairperson, Dr. Ray Taghavi, Date approved: 6/6/2012 ii Abstract This document details the functionality of a software program used to streamline a rocket propulsion system design, analysis and simulation effort. The program aids in unifying the nozzle, chamber and injector portions of a rocket propulsion system design effort quickly and efficiently using a streamlined graphical user interface (GUI). The program also allows for the selection of common nozzle profiles including 80% rao, conical, a user selected percentage bell, and a minimum length nozzle (MLN) using method of characteristics (MOC). Chamber dimensions, propellant selections, and injector selection between doublet or triplet allow for further refinement of the desired rocket system design. The program takes the available selections and specifications made by the user and outputs key design parameters calculated from the input variables. A 2-D graphical representation of the nozzle and/or chamber is plotted and coordinates of the plotted line are displayed. Additional design calculations are determined and displayed within the program such as specific impulse, exhaust velocity, propellant weight flow, fundamental instability frequencies, etc. -
Fuel and Oxidizer Feed Systems
Fuel and Oxidizer Feed Systems Zachary Hein, Den Donahou, Andrew Doornink, Mack Bailey, John Fieler 1 1 Design Selection Recap Fuel Selection Fuel: Ethanol C2H5OH -Potential Biofuel -Low mixture ratio with LOX -Good specific impulse -Easy to get Oxidizer: Liquid Oxygen LOX -Smaller tank needed (Compared to gaseous O2) -Can be pressurized -Lowest oxidizer mixture ratio -Provides Highest specific impulse 2 Design Selection Recap Thrust Chamber Thrust Chamber Selections ● Injector: Like Impinging Doublet ● Cooling System: Regenerative Cooling ● Thrust Chamber Material: Haynes 230 3 Design Selection Recap Thrust Chamber Thrust Chamber Selections ● Injector: Like Impinging Doublet ● Cooling System: Regenerative Cooling ● Thrust Chamber Material: Haynes 230 Huzel, Dieter, and David Huang. "Introduction." Modern Engineering for Design of Liquid-Propellant Rocket Engines. Vol. 147. Washington D.C.: AIAA, 1992. 7-22. Print. 4 Design Selection Recap Thrust Chamber Thrust Chamber Selections ● Injector: Like Impinging Doublet ● Cooling System: Regenerative Cooling ● Thrust Chamber Material: Haynes 230 Huzel, Dieter, and David Huang. "Introduction." Modern Engineering for Design of Liquid-Propellant Rocket Engines. Vol. 147. Washington D.C.: AIAA, 1992. 7-22. Print. http://www.k-makris.gr/RocketTechnology/ThrustChamber/Thrust_Chamber.htm 5 Design Selection Recap Thrust Chamber Thrust Chamber Selections ● Injector: Like Impinging Doublet ● Cooling System: Regenerative Cooling ● Thrust Chamber Material: Haynes 230 Huzel, Dieter, and David Huang. "Introduction." Modern Engineering for Design of Liquid-Propellant Rocket Engines. Vol. 147. Washington D.C.: AIAA, 1992. 7-22. Print. http://www.k-makris.gr/RocketTechnology/ThrustChamber/Thrust_Chamber.htm http://www.alibaba.com/product-detail/haynes-seamless-pipe_1715659362.html 6 Turbo Pump Basics Turbo Pumps provide pressurization to gaseous fuel components to required pressures and mixture ratios. -
Pyridoxine in Clinical Toxicology: a Review Philippe Lheureux, Andrea Penaloza and Mireille Gris
78 Review Pyridoxine in clinical toxicology: a review Philippe Lheureux, Andrea Penaloza and Mireille Gris Pyridoxine (vitamin B6) is a co-factor in many enzymatic controversial. This paper reviews the various indications pathways involved in amino acid metabolism: the main of pyridoxine in clinical toxicology and the supporting biologically active form is pyridoxal 5-phosphate. literature. The potential adverse effects of excessive Pyridoxine has been used as an antidote in acute pyridoxine dosage will also be summarized. intoxications, including isoniazid overdose, Gyromitra European Journal of Emergency Medicine 12:78–85 mushroom or false morrel (monomethylhydrazine) c 2005 Lippincott Williams & Wilkins. poisoning and hydrazine exposure. It is also recommended as a co-factor to improve the conversion of glyoxylic acid European Journal of Emergency Medicine 2005, 12:78–85 into glycine in ethylene glycol poisoning. Other indications Keywords: Antidotes, crimidin, drug-induced neuropathy, ethylene glycol, are recommended by some sources (for example crimidine hydrazine, isoniazid, metadoxine, pyridoxine poisoning, zipeprol and theophylline-induced seizures, adjunct to d-penicillamine chelation), without significant Department of Emergency Medicine, Erasme University Hospital, Brussels, Belgium. supporting data. The value of pyridoxine or its congener Correspondence to Philippe Lheureux, Department of Emergency Medicine, metadoxine as an agent for hastening ethanol metabolism Erasme University Hospital, 808 route de Lennik, 1070 Brussels, Belgium. or improving vigilance in acute alcohol intoxication is E-mail: [email protected] Introduction ing. More controversial issues include alcohol intoxication Pyridoxine or vitamin B6 is a highly water-soluble and zipeprol or theophylline-induced seizures. vitamin. Its main biologically active form is a phosphate ester of its aldehyde form, pyridoxal 5-phosphate (P5P). -
Gyromitrin Poisoning: More Questions Than Answers
Gyromitrin poisoning: more questions than answers Denis R. Benjamin, MD some dedicated mycophagist, who had Many of these clues to the toxin never eaten the mushroom for many years made any coherent sense, even though it “It is perhaps ironic for a mushroom, without any ill effects, would suddenly was known for some years that the toxins Gyromitra esculenta, whose very name and unaccountably take ill. This too could be destroyed by cooking.” (From means edible, to be so poisonous under was passed off as the development of an Benjamin, 1995.) certain circumstances. Surprisingly, allergy in the unfortunate individual, the toxins were only characterized as that the mushrooms had been mistaken ll the enigmas related to this recently as 1968. A number of factors for a poisonous variety, or a rotten toxin remain unresolved. The conspired against the investigators of this batch had been eaten. To compound the current literature merely repeats mushroom poison (Lincoff and Mitchel, difficulties, Gyromitra esculenta caused Awhat was published before 1990. A 1977). The first was the observation that many poisonings in Europe, while in the deluge of “cut and paste.” No meaningful only a few of the participants eating the western USA, the seemingly identical research has been done in the past same quantity of the same mushroom species appeared largely harmless. All three decades. This is due to a number would become ill. Because of this, the sorts of explanations were proposed of factors. The first was the demise of poisoning was immediately ascribed to to explain this discrepancy, including academic pharmacognosy departments, ‘allergy’ or ‘individual idiosyncrasy.’ The such fanciful ones as suggesting that responsible for investigating the biology next problematic observation was that Americans cook their vegetables better. -
Toxicological Profile for Hydrazines. US Department Of
TOXICOLOGICAL PROFILE FOR HYDRAZINES U.S. DEPARTMENT OF HEALTH AND HUMAN SERVICES Public Health Service Agency for Toxic Substances and Disease Registry September 1997 HYDRAZINES ii DISCLAIMER The use of company or product name(s) is for identification only and does not imply endorsement by the Agency for Toxic Substances and Disease Registry. HYDRAZINES iii UPDATE STATEMENT Toxicological profiles are revised and republished as necessary, but no less than once every three years. For information regarding the update status of previously released profiles, contact ATSDR at: Agency for Toxic Substances and Disease Registry Division of Toxicology/Toxicology Information Branch 1600 Clifton Road NE, E-29 Atlanta, Georgia 30333 HYDRAZINES vii CONTRIBUTORS CHEMICAL MANAGER(S)/AUTHOR(S): Gangadhar Choudhary, Ph.D. ATSDR, Division of Toxicology, Atlanta, GA Hugh IIansen, Ph.D. ATSDR, Division of Toxicology, Atlanta, GA Steve Donkin, Ph.D. Sciences International, Inc., Alexandria, VA Mr. Christopher Kirman Life Systems, Inc., Cleveland, OH THE PROFILE HAS UNDERGONE THE FOLLOWING ATSDR INTERNAL REVIEWS: 1 . Green Border Review. Green Border review assures the consistency with ATSDR policy. 2 . Health Effects Review. The Health Effects Review Committee examines the health effects chapter of each profile for consistency and accuracy in interpreting health effects and classifying end points. 3. Minimal Risk Level Review. The Minimal Risk Level Workgroup considers issues relevant to substance-specific minimal risk levels (MRLs), reviews the health effects database of each profile, and makes recommendations for derivation of MRLs. HYDRAZINES ix PEER REVIEW A peer review panel was assembled for hydrazines. The panel consisted of the following members: 1. Dr. -
Synthetic and Naturally Occurring Hydrazines As Possible Cancer Causative Agents
[CANCER RESEARCH 35, 3693-3697 December 1975] Synthetic and Naturally Occurring Hydrazines as Possible Cancer Causative Agents Bela Toth' The Eppley Institute for Research in Cancer, University of Nebraska Medical Center, Omaha, Nebraska 68105 SUMMARY SYNTHETIC HYDRAZINES The various synthetic substituted hydrazines, which cause tumors in animals, are briefly enumerated. To date, 19 of Studies on the carcinogenic potentialities of synthetic them have proved to be tumorigenic in animals. A number substituted hydrazines began in 1962, when it was shown of these chemicals are found today in the environment, in that the base compound hydrazine sulfate induced lung industry, in agriculture, and in medicine, and the human neoplasms in mice (1). Subsequently, a series of hydrazine population is exposed to a certain degree to some of them. derivatives were investigated in various laboratories for Hydrazine also occurs in nature in tobacco and tobacco tumor-inducing capabilities. These studies clearly demon smoke. The three other naturally occurring hydrazine strated that these chemicals are indeed powerful tumori compounds are N-methyl-N-formylhydrazine, which oc genic substances in mice, hamsters, and rats, due to their curs in the wild edible mushroom, Gyromitra esculenta, tumor-inducing abilities in the intestines, brain, lungs, and @-N-[―y-L(+)-glutamylJ-4-hydroxymethylphenyl blood vessels, liver, breasts, kidneys, etc. Now, we know of hydrazine and 4-hydroxymethylphenylhydrazine, whkh 19 hydrazine derivatives that have been shown to be tumor are found in the commonly eaten cultivated mushroom, inducers. These include, in addition to hydrazine (1, 32), Agaricus bisporus. Tumorigenesis studies with the natu methyl- (35, 40), 1,2-dimethyl- (6, 27, 36, 46, 52), 1,1- rally occurring hydrazines are in progress. -
Experimental Study of the Combustion Efficiency in Multi-Element Gas
energies Article Experimental Study of the Combustion Efficiency in Multi-Element Gas-Centered Swirl Coaxial Injectors Seongphil Woo 1,* , Jungho Lee 1,2, Yeoungmin Han 2 and Youngbin Yoon 1,3 1 Department of Aerospace Engineering, Seoul National University, Seoul 08826, Korea; [email protected] (J.L.); [email protected] (Y.Y.) 2 Korea Aerospace Research Institute, Daejeon 34133, Korea; [email protected] 3 Institute of Advanced Aerospace Technology, Seoul National University, Seoul 08826, Korea * Correspondence: [email protected] Received: 27 October 2020; Accepted: 16 November 2020; Published: 19 November 2020 Abstract: The effects of the momentum-flux ratio of propellant upon the combustion efficiency of a gas-centered-swirl-coaxial (GCSC) injector used in the combustion chamber of a full-scale 9-tonf staged-combustion-cycle engine were studied experimentally. In the combustion experiment, liquid oxygen was used as an oxidizer, and kerosene was used as fuel. The liquid oxygen and kerosene burned in the preburner drive the turbine of the turbopump under the oxidizer-rich hot-gas condition before flowing into the GCSC injector of the combustion chamber. The oxidizer-rich hot gas is mixed with liquid kerosene passed through combustion chamber’s cooling channel at the injector outlet. This mixture has a dimensionless momentum-flux ratio that depends upon the dispensing speed of the two fluids. Combustion tests were performed under varying mixture ratios and combustion pressures for different injector shapes and numbers of injectors, and the characteristic velocities and performance efficiencies of the combustion were compared. It was found that, for 61 gas-centered swirl-coaxial injectors, as the moment flux ratio increased from 9 to 23, the combustion-characteristic velocity increased linearly and the performance efficiency increased from 0.904 to 0.938.