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144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,545 | 1.A.1. Complete rocket systems (including ballistic missile systems, space launch vehicles, and sounding rockets) capable of delivering at least a 500 kg "payload" to a "range" of at least 300 km. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,546 | 1.A.2. Complete unmanned aerial vehicle systems (including cruise missile systems, target drones and reconnaissance drones) capable of delivering at least a 500 kg "payload" to a "range" of at least 300 km. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,547 | 1.B.1. "Production facilities" specially designed for the systems specified in 1.A. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,548 | 1.D.1. "Software" specially designed or modified for the "use" of "production facilities" specified in 1.B. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,549 | 1.D.2. "Software" which coordinates the function of more than one subsystem, specially designed or modified for "use" in systems specified in 1.A. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,550 | 1.E.1. "Technology", in accordance with the General Technology Note, for the "development", "production" or "use" of equipment or "software" specified in 1.A., 1.B., or 1.D. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,551 | 2.A.1. Complete subsystems usable in the systems specified in 1.A. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,552 | Individual rocket stages usable in the systems specified in 1.A. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,553 | Re-entry vehicles, and equipment designed or modified therefor, usable in the systems specified in 1.A., as follows, except as provided in the Note below 2.A.1. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,554 | Solid propellant rocket motors or liquid propellant rocket engines, usable in the systems specified in 1.A., having a total impulse capacity equal to or greater than 1. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,555 | Liquid propellant apogee engines and station-keeping engines specified in 2.A.1.c., designed or modified for use on satellites, may be treated as Category II, if the subsystem is exported subject to end-use statements and quantity limits appropriate for the excepted end-use stated above, when having a vacuum thrust not greater than 1kN. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,556 | 'Guidance sets', usable in the systems specified in 1.A., capable of achieving system accuracy of 3.33% or less of the "range" (e.g. a 'CEP' of 10 km or less at a "range" of 300 km), except as provided in the Note below 2.A.1. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,557 | A ´guidance set´ integrates the process of measuring and computing a vehicle's position and velocity (i.e. navigation) with that of computing and sending commands to the vehicle's flight control systems to correct the trajectory. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,558 | ´CEP´ (circle of equal probability) is a measure of accuracy, defined as the radius of the circle centred at the target, at a specific range, in which 50% of the payloads impact. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,559 | Thrust vector control sub-systems, usable in the systems specified in 1.A., except as provided in the Note below 2.A.1. for those designed for rocket systems that do not exceed the "range"/"payload" capability of systems specified in 1.A. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,560 | Use of thrust tabs. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,561 | Weapon or warhead safing, arming, fuzing, and firing mechanisms, usable in the systems specified in 1.A., except as provided in the Note below 2.A.1. for those designed for systems other than those specified in 1.A. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,562 | The exceptions in 2.A.1.b., 2.A.1.d., 2.A.1.e. and 2.A.1.f. above may be treated as Category II if the subsystem is exported subject to end-use statements and quantity limits appropriate for the excepted end-use stated above. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,563 | 2.B.1. "Production facilities" specially designed for the subsystems specified in 2.A. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,564 | 2.B.2. "Production equipment" specially designed for the subsystems specified in 2.A. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,565 | 2.D.1. "Software" specially designed or modified for the "use" of "production facilities" specified in 2.B.1. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,566 | 2.D.2. "Software" specially designed or modified for the "use" of rocket motors or engines specified in 2.A.1.c. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,567 | 2.D.3. "Software", specially designed or modified for the "use" of 'guidance sets' specified in 2.A.1.d. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,568 | 2.D.3. includes "software", specially designed or modified to enhance the performance of ´guidance sets´ to achieve or exceed the accuracy specified in 2.A.1.d. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,569 | 2.D.4. "Software" specially designed or modified for the "use" of subsystems or equipment specified in 2.A.1.b.3. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,570 | 2.D.5. "Software" specially designed or modified for the "use" of systems in 2.A.1.e. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,571 | 2.D.6. "Software" specially designed or modified for the "use" of systems in 2.A.1.f. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,572 | Subject to end-use statements appropriate for the excepted end-use, "software" controlled by 2.D.2. - 2.D.6. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,573 | Under 2.D.2. if specially designed or modified for liquid propellant apogee engines, designed or modified for satellite applications as specified in the Note to 2.A.1.c. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,574 | Under 2.D.5. if designed for rocket systems that do not exceed the "range" "payload" capability of systems specified in 1.A. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,575 | Under 2.D.6. if designed for systems other than those specified in 1.A. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,576 | 2.E.1. "Technology", in accordance with the General Technology Note, for the "development", "production" or "use" of equipment or "software" specified in 2.A., 2.B. or 2.D. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,577 | Maximum thrust value greater than 400 N (achieved un-installed) excluding civil certified engines with a maximum thrust value greater than 8. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,578 | Specific fuel consumption of 0. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,579 | Engines designed or modified for systems specified in 1.A. or 19.A.2., regardless of thrust or specific fuel consumption. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,580 | Engines specified in 3.A.1. may be exported as part of a manned aircraft or in quantities appropriate for replacement parts for a manned aircraft. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,581 | 3.A.2. Ramjet/scramjet/pulse jet/combined cycle engines, including devices to regulate combustion, and specially designed components therefor, usable in the systems specified in 1.A. or 19.A.2. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,582 | 3.A.3. Rocket motor cases, 'insulation' components and nozzles therefor, usable in the systems specified in 1.A. or 19.A.1. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,583 | In 3.A.3. ´insulation´ intended to be applied to the components of a rocket motor, i.e. the case, nozzle inlets, case closures, includes cured or semi-cured compounded rubber components comprising sheet stock containing an insulating or refractory material. It may also be incorporated as stress relief boots or flaps. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,584 | Refer to 3.C.2. for ´insulation´ material in bulk or sheet form. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,585 | 3.A.4. Staging mechanisms, separation mechanisms, and interstages therefor, usable in the systems specified in 1.A. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,586 | 3.A.5. Liquid and slurry propellant (including oxidisers) control systems, and specially designed components therefor, usable in the systems specified in 1.A., designed or modified to operate in vibration environments greater than 10 g rms between 20 Hz and 2 kHz. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,587 | The only servo valves and pumps specified in 3.A.5. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,588 | Servo valves designed for flow rates equal to or greater than 24 litres per minute, at an absolute pressure equal to or greater than 7 MPa, that have an actuator response time of less than 100 ms. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,589 | Pumps, for liquid propellants, with shaft speeds equal to or greater than 8,000 rpm or with discharge pressures equal to or greater than 7 MPa. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,590 | Systems and components specified in 3.A.5. may be exported as part of a satellite. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,591 | 3.A.6. Hybrid rocket motors and specially designed components therefor, usable in the systems specified in 1.A., 19.A.1. or 19.A.2. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,592 | c. A width between 10 and 20 mm. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,593 | 3.A.8. Liquid propellant tanks specially designed for the propellants controlled in Item 4.C. or other liquid propellants used in the systems specified in 1.A.1. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,594 | 3.A.9. 'Turboprop engine systems' specially designed for the systems in 1.A.2. or 19.A.2., and specially designed components therefor, having a maximum power greater than 10 kW (achieved uninstalled at sea level standard conditions), excluding civil certified engines. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,595 | For the purposes of Item 3.A.9. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,596 | b. Power transmission system to transfer the power to a propeller. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,597 | 3.B.1. "Production facilities" specially designed for equipment or materials specified 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. or 3.C. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,598 | 3.B.2. "Production equipment" specially designed for equipment or materials specified 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. or 3.C. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,599 | Have more than two axes which can be co-ordinated simultaneously for contouring control. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,600 | Machines combining the function of spin-forming and flow-forming are, for the purpose of this item, regarded as flow-forming machines. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,601 | This item does not include machines that are not usable in the "production" of propulsion components and equipment (e.g. motor cases) for systems specified in 1.A. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,602 | 3.C.1. 'Interior lining' usable for rocket motor cases in the systems specified in 1.A. or specially designed for systems specified in 19.A.1. or 19.A.2. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,603 | In 3.C.1. ´interior lining´ suited for the bond interface between the solid propellant and the case or insulating liner is usually a liquid polymer based dispersion of refractory or insulating materials e.g. carbon filled HTPB or other polymer with added curing agents to be sprayed or screeded over a case interior. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,604 | 3.C.2. 'Insulation' material in bulk form usable for rocket motor cases in the systems specified in 1.A. or specially designed for systems specified in 19.A.1. or 19.A.2. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,605 | In 3.C.2. ´insulation´ intended to be applied to the components of a rocket motor, i.e. the case, nozzle inlets, case closures, includes cured or semi-cured compounded rubber sheet stock containing an insulating or refractory material. It may also be incorporated as stress relief boots or flaps specified in 3.A.3. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,606 | 3.D.1. "Software" specially designed or modified for the "use" of "production facilities" and flow forming machines specified in 3.B.1. or 3.B.3. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,607 | 3.D.2. "Software" specially designed or modified for the "use" of equipment specified in 3.A.1., 3.A.2., 3.A.4., 3.A.5., 3.A.6. or 3.A.9. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,608 | "Software" specially designed or modified for the "use" of engines specified in 3.A.1. may be exported as part of a manned aircraft or as replacement "software" therefor. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,609 | "Software" specially designed or modified for the "use" of propellant control systems specified in 3.A.5. may be exported as part of a satellite or as replacement "software" therefor. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,610 | 3.D.3. "Software" specially designed or modified for the "development" of equipment specified in 3.A.2., 3.A.3. or 3.A.4. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,611 | 3.E.1. "Technology", in accordance with the General Technology Note, for the "development", "production" or "use" of equipment, materials or "software" specified in 3.A.1., 3.A.2., 3.A.3., 3.A.4., 3.A.5., 3.A.6., 3.A.9., 3.B., 3.C. or 3.D. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,612 | 4.B.1. "Production equipment", and specially designed components therefor, for the "production", handling or acceptance testing of liquid propellants or propellant constituents specified in 4.C. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,613 | 4.B.2. "Production equipment", other than that described in 4.B.3., and specially designed components therefor, for the production, handling, mixing, curing, casting, pressing, machining, extruding or acceptance testing of solid propellants or propellant constituents specified in 4.C. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,614 | a. Batch mixers with provision for mixing under vacuum in the range of zero to 13. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,615 | b. Continuous mixers with provision for mixing under vacuum in the range of zero to 13. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,616 | c. Fluid energy mills usable for grinding or milling substances specified in 4.C. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,617 | d. Metal powder "production equipment" usable for the "production", in a controlled environment, of spherical or atomised materials specified in 4.C.2.c., 4.C.2.d. or 4.C.2.e. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,618 | c. Equipment usable for the "production" of spherical aluminium powders by powdering a melt in an inert medium (e.g. nitrogen). |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,619 | The only batch mixers, continuous mixers, usable for solid propellants or propellants constituents specified in 4.C., and fluid energy mills specified in 4.B., are those specified in 4.B.3. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,620 | Forms of metal powder "production equipment" not specified in 4.B.3.d. are to be evaluated in accordance with 4.B.2. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,621 | 4.C.1. Composite and composite modified double base propellants. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,622 | A particle size of 63 µm (ISO R-565) corresponds to 250 mesh (Tyler) or 230 mesh (ASTM standard E-11). |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,623 | The natural content of hafnium (CAS 7440-58-6) in the zirconium (typically 2% to 7%) is counted with the zirconium. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,624 | f. High energy density materials such as boron slurry, having an energy density of 40 x 106 J/kg or greater. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,625 | Perchlorates, chlorates or chromates mixed with powdered metals or other high energy fuel components. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,626 | Mixed Oxides of Nitrogen (MON) are solutions of Nitric Oxide (NO) in Dinitrogen Tetroxide/Nitrogen Dioxide (N2O4/NO2) that can be used in 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 of Nitric Oxide in the mixture (e.g. MON3 contains 3% Nitric Oxide, MON25 25% Nitric Oxide. An upper limit is MON40, 40% by weight). |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,627 | Item 4.C.4.a.6. does not control Nitrogen Trifluoride (NF3) (CAS 7783-54-2) in a gaseous state as it is not usable for missile applications. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,628 | f. Polytetrahydrofuran polyethylene glycol (TPEG). |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,629 | Polytetrahydrofuran polyethylene glycol (TPEG) is a block co-polymer of poly 1,4-Butanediol and polyethylene glycol (PEG). |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,630 | N-methyl-p-nitroaniline (CAS 100-15-2). |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,631 | 4.D.1. "Software" specially designed or modified for the "use" of equipment specified in 4.B. for the "production" and handling of materials specified in 4.C. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,632 | 4.E.1 "Technology", in accordance with the General Technology Note, for the "development", "production" or "use" of equipment or materials specified in 4.B. and 4.C. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,633 | 6.A.1. Composite structures, laminates, and manufactures thereof, specially designed for use in the systems specified in 1.A., 19.A.1. or 19.A.2. and the subsystems specified in 2.A. or 20.A. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,634 | 6.A.2. Resaturated pyrolised i.e. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,635 | Usable in the systems specified in 1.A. or 19.A.1. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,636 | 6.B.1. Equipment for the "production" of structural composites, fibres, prepregs or preforms, usable in the systems specified in 1.A., 19.A.1. or 19.A.2. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,637 | 6.B.1.c. does not control textile machinery not modified for the end-uses stated. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,638 | e. Equipment designed or modified for special fibre surface treatment or for producing prepregs and preforms, including rollers, tension stretchers, coating equipment, cutting equipment and clicker dies. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,639 | Examples of components and accessories for the machines specified in 6.B.1. are moulds, mandrels, dies, fixtures and tooling for the preform pressing, curing, casting, sintering or bonding of composite structures, laminates and manufactures thereof. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,640 | 6.B.2. Nozzles specially designed for the processes referred to in 6.E.3. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,641 | c. Possessing a chamber cavity with an inside diameter of 254 mm or greater. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,642 | 6.B.4. Chemical vapour deposition furnaces designed or modified for the densification of carbon-carbon composites. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,643 | 6.B.5. Equipment and process controls, other than those specified in 6.B.3. or 6.B.4., designed or modified for densification and pyrolysis of structural composite rocket nozzles and re-entry vehicle nose tips. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,644 | 6.C.1. Resin impregnated fibre prepregs and metal coated fibre preforms, for the goods specified in 6.A.1., made either with organic matrix or metal matrix utilising fibrous or filamentary reinforcements having a specific tensile strength greater than 7.62 x 104 m and a specific modulus greater than 3.18 x 106 m. |
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