prop · GE0397 · 1990-12-31 00:00:00 — Completerocket systems (including ballistic missile systems, space launch vehicles, andsounding rockets) and unmanned air vehicle systems (including craise missile systems,target drones, and reconnaissance drones) capable of delivering at least a payload to a range of at least as well as the specially designedproduction facilities for these systems. Completesubsystems usable in the systems in item I, as follows, as well as thespecially designed production facilities and production equipment therefor: (a) Individual rocket stages; (b) Reentry vehicles, and specially designed equipmenttherefor, as follows, except as provided in note (1) below for those designedfor non-weapons payloads: (1) Heat shields and components thereof fabricated of ceramic or ProD 1990/91 "97 (2) Heatsinks and components thereof fabricated of light-weight, .' highheat capacity materials; ° (3) Electronicequipment specially designed or modified for reentry vehicles. (c) Solidor liquid fuel rocket engines, having a total impulse capacity of 2.5x10' Ib-sec or greater, except as provided in note (1) below for those specially designed or modified for orbital correction of satelli- tes; (d) Guidancesets capable of achieving system accuracy (CEP) of or less at a range of , except as provided in note (1) below for those designed for missiles with range or manned aircraft; (e) Thrastvector controls, except as provided in note (1) below for those designed for rocket systems with range ; (f) Warheadsafing, arming, fuzing, and firing mechanisms, except as provided in note (1) below for those designed for systems other than those in Item 1. Notesto Item 2: (1) The exceptions in (b), (c), (d), (e), and (O above may be treated asCategory II if the subsystem is exported subject to end use statements andquantity limits appropriate for the excepted end use stated above. (2) CEP (circle of equal probability) is a measure of accuracy; the radiusof the circle centered at the target, at a specific range, in which 50 percentof the payloads impact. Propulsioncomponents and equipment usable in the systems in Item 1, as follows, as wellas the specially designed production facilities therefor: (a) Lightweight turbojet and turbofan engines(including turbocom-pound engines) that are small and fuel efBcient; (b) Ramjet/Scramjet engines, including devices to regulatecombustion, and specially designed production equipment therefor; (c) Rocket motor cases and specially designedproduction equipment therefor; (d) Stagingmechanisms and specially designed production equipment therefor; (e) Liquidfuel control systems and components therefor, specially desig ned to operate in vibrating environments of more than rms between 20 H and 2000 H including: (1)Servo valves designed for flow råtes of 24 litres per minute or greater at apressure of 250 bars, and having flow contact surfaces made of 90 percent ormore tantalum, titanium or zirconium, ProD1990/91 "97 either separately or combined, except when such surfacesare . ' madeof materials contain ing more than 97 percent and less than ° (2) Pumps (except vacuum pumps), having all flow contact surfaces madeof 90 percent or more tantalum, titanium or zirconium, eitherseparately or combined, except when such surfaces are madeof mate rials containing more than 97 percent and less than Notesto Item 3: (1) Item3(a) engines may be exported as part of a manned aircraft or in quantities appropriate for replacement parts for manned air craft. (2) Item3(e) systems and components may be exported as part of a satellite. ITEM4-CA TEGOR Y H Propellantsand constituent chemicals for propellants as follows: (a) Propulsivesubstances: (1) Hydrazinewith a concentration of more than 70 percent; (2) Unsymmetric dimethylhydrazine (UDMH); (3) Spherical ammonium perchlorate with particles ofuniform diameter less than 500 microns; (4) Spherical aluminum powder with particles of uniformdiameter of less than 500 microns and an aluminium content of 97 percent orgreater; (5) Metal fuels in particle sizes less than 500microns, whether spherical, atomized, spheroidal, flaked or ground, consistingof 97 percent or more of any of the following: zirconium, titanium, uranium,tungsten, boron, zinc, and alloys of these; magnesium; Misch metal; (6) Nitro-amines (cyclotetramethylenetetranitramine(HMX), cyc-lotetramethylenetrinitramine (RDX)) when specially formula-ted aspropulsive substances. (b) Polymeric substances: (1) Carboxy-terminated polybutadiene (CTPB); (2) Hydroxy-terminated polybutadiene (HTPB); (c) Compositepropellants including molded glue propellants and propel lants with nitrated bonding and aluminum content in excess of 5 percent. (d) Otherhigh energy density fuels such as Boron Slurry, having an energy density of 40x 10* joules/kg or greater. ITEM5- CATEGORYH Prop. Productiontechnoloy or production equipment specially designed or mo- tJiiaga odified for production, handling, mixing, curing, casting, pressing, machi-ningand acceptance testing of the liquid or solid propellants and propel-lantconstituents as described in Item 4. ITEM6 - CATEGORY II Equipment,technical data and procedures for the production of stmctural composites usablein the systems in Item 1 as follows, and specially designed components andaccessories and specially designed software therefor: (a) Filament winding of which the motions forpositioning, wrapping and winding fibres are coordinated and programmed inthree or more axes, specially designed to fabricate composite strac-tures orlaminates from fibrous and filamentary materials; and coor-dinating andprogramming controls; (b) Tape-laying of which the motions forpositioning and laying tape and sheets are coordinated and programmed in two ormore axes, specially designed for the manufacture of composite airframes andmissile stractures; (c) Interlacing , including adapters andmodification kils for weaving, interlacing or braiding fibres to fabricatecomposite stractures, except textile machinery which has not been modified forthe above end-uses; (d) Speciallydesigned or adapted equipment for the production of fibro us and filamentary materials as follows: (1) Equipment for converting polymeric fibers (such aspolyacrylonitrile, rayon, or polycarbosilane) including special provision tostrain the fibre during heating; (2) Equipment for the vapor deposition of elements orcompounds on heated filamentary substrates; and (3) Equipment for the wet-spinning of refractoryceramics (such as aluminum oxide); (e) Speciallydesigned or adapted equipment for special fibre surface treatment or for producing prepregs and preforms. Note: Equipment covered by this sub-item includes but is not limited to rollers, tension stretchers, coating equipment, cutting equipment and clicker dies. (O Technical data(including processing conditions) and procedures for the regulation oftemperature, pressures or atmosphere in autoclaves when used for the productionof composites or partially processed composites. Note to Item 6: Speciallydesigned or adapted components and accessories for the covered bythis entry include, but are not limited to, moulds, man- drels,dies, fixtures and tooling for the preform pressing, curing, casting, Prop.1990/91:97 sintering or bonding of composite structures, laminates andmanufactures Bilaga 6 thereof ITEM7 - CATEGORY 11 Pyrolyticdeposition and densification equipment and technology as follows: (a) Technology for producing pyrolytically derivedmaterials formed on a mold,mandrel or other substrate from precursor gaseswhich decom-pose in the to temperature range at pressures of I mmHg to (including technology for the composition of precursor gases,flow-rates, and process control schedules and parameters); (b) Specially designed nozzles for the above processes; (c) Equipment and process controls, and speciallydesigned software therefor, specially designed for densification and pyrolysisof struc-tural composite rocket nozzles and reentry vehicle nose tips. Structuralmaterials usable in the systems in Item 1, as follows: (a) Composite structures, laminates, and manufacturesthereof including resin impregnated fibre prepregs and metal coated fibrepreforms therefor, specially designed for use in the systems in Item 1 and thesubsystems in Item 2 made either with an organic matrix or metal matrixutilizing fibrous or filiamentary reinforcements having a specific tensilestrength greater than 7.62 X10" m (3x10'' inches) and aspecific modulus greater than 3. 18x 10* m (1.25x10* inches); (b) Resaturated pyrolized (i.e., carbon-carbon) materialsspecially designed for rocket systems; (c) grain artificial graphites for rocket nozzlesand reentry vehicle nosetips having all of the following characteristics:(l)Bulkdensity of 1.79 or greater (measured at 293 K); (2)Tensile strain to failure of 0.7 percent or greater (measured at 293K);(3)Coefficient of thermal expansion of 2.75x lO* or less per degree K (intherangeof293Kto1,255K); (d) Ceramiccomposite materials specially designed for use in missile radomes. Compasses,gyroscopes, accelerometers and inertial equipment and specially designedsoftware therefor, as follows; and specially designed components thereforusable in the systerns in Item I: (a) Integrated flight instrument systems which include gyrostabilizers or 72 ProD1990/91 "97 automatic pilots and integration software therefor, speciallydesigned /- ormodified for use in the systems in Item I; ° (b) Gyro-astro compasses and other devices which deriveposition or orientation by means of automatically tracking celestial bodies; (c) Accelerometers with a threshold of or less,or a linearity error within 0.25 percent~X)f full scale output or both, whichare designed for use in inertial navigation systems or in guidance systems ofall types; (d) Gyroswith a rated free directional drift råte (rated free precession) of. less than 0.5 degree (1 sigma or rms) per hour in a environment; (e) Continuousoutput accelerometers which utilize servo or force balan- ce techniques and gyros, both specified to function at acceleration levels greater than ; (OInertial or other equipment using accelerometers described by subi-tems (c) and(e) above or gyros described by subitems (d) or (e) above, and systemsincorporating such equipment, and specially designed integration softwaretherefor; (g)Specially designed test, calibration, and alignment equipment for the above; (h)Specially designed production equipment for the above, including the following: (1) Forring laser gyro equipment, the following equipment used to characterize mirrors, having the threshold accuracy shown or bet- ter: (i) Rectilinear Scatterometer (10 ppm); (ii) Polar Scatterometer (10 ppm);(iii) Reflectometer (50 ppm); (iv) Profilimeter (5 ); (2) Forother inertial equipment: (i) InertialMeasurement Unit (IMU Module) Tester; (ii) IMUPlatform Tester; (iii) IMUStable Element Handling Fixture; (iv) IMUPlatform Balance Fixture; (v) GyroTuning Test Station; (vi) GyroDynamic Balance Station; (vii) Gyro Run-In/MotorTest Station; (viii) GyroEvacuation and Fill Station; (ix) CentrifugeFixture for Gyro Bearings; (x) AccelerometerAxis Align Station; (xi) AccelerometerTest Station. Noteto Item 9: Items (a) through (O may be exported as part of a manned aircraft orsatellite or in quantities appropriate for replacement parts for mannedaircraft. 6 1990/91. ITEMIO- CATEGORYII Prop. Flightcontrol systems usable in the systems in Item 1 as follows, as well as 'lägao the specially designed test, calibration, and alignment equipment therefor: (a) Hydraulic, mechanical, electro-optical, orelectro-mechanical flight control systems (including fly-by-wire systems)specially designed or modified for the systems in Item 1; (b) Attitude control equipment specially designed ormodified for the systems in Item 1; (c) Design technology for integration of air vehiclefuselage, propulsion system and lifting and control surfaces to optimizeaerodynamic performance throughout the flight regime of an unmanned air vehicle; (d) Designtechnology for integration of flight control, guidance, and propulsion data into a flight management system for optimization of rocket system trajectory. Noteto Item 10: Items (a) and (b) may be exported as part of a manned aircraft orsatellite or in quantities appropriate for replacement parts for mannedaircraft. ITEMII - CATEGORY H Avionicsequipment specially designed or modified for use in unmanned air vehicles orrocket systems and specially designed software and components therefor usablein the systems in Item 1, including but not limited to: (a) Radar and laser radar systems, includingaltimeters; (b) Passive sensors for determining bearing to specificelectromagnetic sources (direction finding equipment)or terraincharacteristics; (c) Equipment specially designed for real-timeintegration, processing, and use of navigation information derived from anexternal source; (d) Electronicassemblies and components specially designed for military use incorporating any of the following: (1) Speciallydesigned, integral stractural supports; (2) Techniques for conductive heat removal; (3) Radiation hardening; (4) Design for reliable short term operation attemperatures in excess of ; (e) Designtechnology for protection of avionic and electrical subsystems against electromagnetic pulse (EMP) and electromagnetic interferen- ce () hazards from external sources, as follows: (1) Technology for design of shielding systems; (2) Technology for the configuration design of hardenedelectrical circuits and subsystems; (3) Determination of hardening criteria for the above. Notesto Item II: (1) Item 11 equipment may be exported as part of a manned aircraft or 74 ProD1990/91 "97 satellite or in quantities appropriate for replacement parts for man- ' (2) Examples of equipment included in this item: Terraincontour mapping equipment; Scenemapping and correlation (both digital and analog) equipment; Dopplernavigation radar equipment; Imagingsensor equipment (both and passive). Launchand ground support equipment and facilities usable for the systems in Item I,as follows: (a) Apparatus and devices specially designed ormodified for the handling, control, activation and launching of the systems inItem 1; (b) Military vehicles specially designed or modifiedfor the handling, control, activation and launching of the systems in Item 1; (c) Gravity meters (gravimeters), gravity gradiometers,and specially designed components therefor, designed or modified for airborneor use, and having a static or operational accuracy of one milligal orbetter, with a time to steady-state registration of two minutes or less; (d) Telemeteringand telecontrol equipment suitable for use with unman ned air vehicles or rocket systems; (e) Precisiontracking systems: (1) Tracking systems which use a translator installedon the rocket system or unmanned air vehicle in conjunction with either surfaceor airborne references or navigation satellite systems to provide real-timemeasurements of inflight position and velocity; (2) Software systems which process recorded data forpost mission precision tracking enabling determination of vehicle position. Analogcomputers, digital computers, or digital differential analyzers speciallydesigned or modified for use in air vehicles or rocket systems and usable inthe systems in Item 1, having any of the following characteristics: (a) Rated for continuous operation at temperatures frombelow to above ; (b) Designed as raggedized or radiation hardenedequipment and capable of meeting military specifications for raggedized orradiation-harde-ned equipment; or, (c) Modified for military use. Noteto Item 13: Item 13 equipment may be exported as part of a manned aircraft or satellite or in quantities appropriate for replacement parts for manned aircraft. ITEM 14 - CA TEGOR YII Prop. Analog-to-digitalconverters, other than digital voltmeters or counters, ""ga o usablein the systems in Item I and having any of the following characteristics:rated for continuous operation at temperatures from below to above55''C; designed to meet military specifications for raggedized equipment, ormodified for military use; or designed for radiation resistance, as follows: (a) Electricalinput type analog-to-digital converters having any of the following characteristics: (1) A conversion råte of more than 200,000 completeconversions per second at rated accuracy; (2) An accuracy in excess of 1 part in more than 10,000of full scale över the specified operating temperature range; (3) A figure of merit of I x 1 O* or more (derived fromthe number of complete conversions per second divided by the accuracy). (b) Analog-to-digitalconverter microcircuits having both of the following characteristics: (1) A maximum con version time to maximum resolution ofless than 20 microseconds; (2) A rated non-linearity of better than 0.025 percentof full scale över the specified operating temperature range. Testfacilities and equipment usable for the systems in Item I, as follows: (a) Vibration test equipment using digital controltechniques and specially designed ancillary equipment and software thereforcapable of imparting forces of 100 kN (22,500 Ibs) or greater; (b) Supersonic (Mach 1.4 to Mac.h5), hypersonic (Mach 5to Mach 15), and hypervelocity (above Mach 15) wind tunnels, except thosespecially designed for educational purposes and having a test section size(measured internally) of less than (10 inches); (c) Test benches with the capacity to handle solid orliquid fuel rockets of more than 20,000 Ibs of thrast, and capable of measuringthe three thrast components. Noteto Item I5(a): The term "digital control" refers to equipment, thefunctions of which are, partly or entirely, automatically controlled by storedand digitally coded electrical signals. Speciallydesigned software, or specially designed software and related specially designed analog or hybrid (combined analog/digital) computers, for modeling, simulation, or design integration of rocket systems and unmanned air vehicle systems, usable for the systems in Item 1. ITEM 17 - CATEGORYII Prop. Technology,materials, and devices for reduced observables such as radar reflectivity,optical/infrared signatures and acoustic signatures (i.e., stealth technology),for military application in rocket systems and unmanned air vehicles, andusable for the systems in Hem I, for example: (a) Stractural materials and coatings speciallydesigned for reduced radar reflectivity; (b) Optical coatings, including paints, speciallydesigned or formulated for reduced optical relflection or emissivity, exceptwhen specially used for thermal control of satellites. ITEM18 -CA TEGOR Y11 Technologyand devices specially designed for use in protecting rocket systems andunmanned air vehicles against nuclear effects (e.g., Electromagnetic Pulse(EMP), X-rays, combined blast and thermal effects), and usable for the systemsin Item 1, for example: (a) Hardenedmicrocircuits and detectors specially designed to withstand radiation as follows: (1) Neutron dosage of 1 x 10' neutrons/cm- (singleevent); (2) Gamma dose råte of 1 x 10' rads/sec; (3) Total dose 1500 rads (single event). (b) Radomesspecially designed to withstand a combined thermal shock greater than 100 cal/cm accompanied by a peak overpressure of greater than per square inch. Noteto Hem I8(a): A microcircuit is defined as a device in which a number ofpassive and circuit elements are considered as indivisibly associated onor within a continuous stracture to perform tshe function of a circuit. Departementspromemorians redogörelse för imple- Pop.1990/91:97 mentering av MTCR-regimen bilaga i 1Amerikas Förenta Stater har MTCR implementerats i där gällandeexportkontrollregimer. Om militära komponenter ingår, följs InternationalTraffic Arms Regulation. Tillstånd lämnas av State Department. Omdual-useprodukter, dvs. produkter med både civil och militär användning, ingårgäller Regulation och ansökan prövas av Department ofCommerce. I båda fallen remissbehandlas ärendet av och informella samråd äger normalt mm mellan berörda instanser. 1C a n a d a regleras exporten av missiler m.m. liksom bl. a. krigsmaterieloch kärnteknologi - av Export and Imports Permits Act. I anslutning till lagenfinns en särskild Export Control List, som anger produkter för vilkaexporttillstånd krävs. Listanupptar de i MTCR-annexet angivna produkterna och teknologin. Policyfrågorbereds inom Arms Control and Disarmament Division och tillståndsfrågor inomExport Controls Division () inomutrikesministeriet i nära samråd med försvarsministeriet. Beslutanderätten närdet gäller missilfrågor ligger hos utrikesministern som vid behov konsulterarandra ledamöter av regeringen. IStorbritannienkontrolleras exporten på samma sätt som krigsmateriel, högteknologi, vissakemiska produkter m. m. enligt the Export of Goods (Control) Order. Varuområdetfanns dock redan tidigare på den av tilllämpade COCOM-listan. Påbasis av MTCR har kontrollen på missilområdet utsträckts till att omfatta flerländer och fått en mer restriktiv tillämpning . Frågor om export avkontrollerade varuområden prövas gemensamt av ,och Foreign and Commonwealth Office. Exportenav missiler m.m. behandlas i på samma sätt som export avkrigsmateriel. Ansökan om exporttillstånd ges in till le Secréta-riat Generalpour la Défense Nationale (SGDN), som lyder under premiärministern. Därefterbereds ärendet inom la Commission Interministerielle pour PEtude desExportations de Matériels de Guerre. Yttranden inhämtas från utrikes-,ekonomi- och försvarsministeriema, som alla är representerade i kommissionen.Besluten fattas formellt av generalsekreteraren i SGDN. Behandlingeni av missilärenden följer i princip reglerna för krigsmaterielexport. Beslut om utförsel m.m. fattas av . Ärendena bereds av en statlig myndighet, Bundesamt fur Aussenwirtschaft. Inom hand läggs frågoma av Auswärtiges Amt tillsammans med ekonomiministeriet. Varor som klassificeras som krigsmateriel finns upptagna dels i Kriegswaf- fenliste bilagd till Kriegswaffenkontrollgesetz, dels i Ausfuhrliste bilagdtill Aussenwirtschaftsgesetz med Aussenhandelsverordnung. Ausfuhrliste be står av fyra listor, nämligen (A) vapen, ammunition, mstningsvaror, (B) kärnenergiutmstning, (C) civila varor och teknologi av strategisk betydelse 78 (dual-useprodukter)samt (D) utrustning för den kemiska industrin. 1990/91:97 MTCR-listanär, allt efter produktens utformning, inarbetad i nyssnämn- Bilaga 7 dalistor, företrädesvis i Kriegswaffenliste samt listorna A och C. Ansvaretför missilkontrollen åvilar i 11 a I i e n, på motsvarande sätt som när detgäller vapenexporten, utrikesministeriets ekonomiska avdelning ochutrikeshandelsministeriet. En interministeriell kommitté granskar inkomnaansökningar om export resp. utländskt samarbete på missilområdet och gerrekommendation om beslut. Till sin hjälp har den interministeriella kommitténen teknisk underkommitté med representanter från i första hand flygvapnet. 1Japan hanteras MTCR enligt lagen om kontroll av utländsk valuta och utrikeshandel (the Trade Control ) och enligtregeringens direktiv rörande exportkontroll resp. valutakontroll. Kontrollistanär inkluderad i det japanska exportkontrolldirektivet innehållande ett stortantal varugrupper. Underlag för regeringens beslut bereds inom finans-,utrikeshandels och industridepartementen, men även andra departement deltar. Departementspromemoriansredogörelse för kon- Prop-1990/91:97 trollåtgärder inom Bilaga 8 Flertalet av länderna har dock infört utförselkontroll. Detta harskett antingen i form av ett generellt utförselförbud med krav på tillstånd förutförsel till alla länder, eller i form av ett begränsat förbud med krav påtillstånd för utförsel till vissa länder. Kombinationer förekommer också på såsätt att ett förbud kan gälla generellt beträffande vissa ämnen, medan ettförbud beträffande andra ämnen kan vara begränsat till att endast avse utförseltill vissa länder.