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144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,645 | The only resin impregnated fibre prepregs specified in 6.C.1. are those using resins with a glass transition temperature (Tg), after cure, exceeding 145oC as determined by ASTM D4065 or national equivalents. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,646 | In Item 6.C.1. 'specific tensile strength' is the ultimate tensile strength in N/m2 divided by the specific weight in N/m3, measured at a temperature of (296 ± 2)K ((23 ± 2)°C) and a relative humidity of (50 ± 5)%. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,647 | In Item 6.C.1. 'specific modulus' is the Young's modulus in N/m2 divided by the specific weight in N/m3, measured at a temperature of (296 ± 2)K ((23 ± 2)°C) and a relative humidity of (50 ± 5)%. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,648 | 6.C.2. Resaturated pyrolised i.e. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,649 | Usable in the systems specified in 1.A. or 19.A.1. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,650 | 6.C.3. Fine grain graphites with a bulk density of at least 1. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,651 | Blocks having a size of 120 mm x 120 mm x 50 mm or greater. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,652 | 6.C.4. Pyrolytic or fibrous reinforced graphites usable for rocket nozzles and re-entry vehicle nose tips usable in systems specified in 1.A. or 19.A.1. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,653 | 6.C.5. Ceramic composite materials (dielectric constant less than 6 at any frequency from 100 MHz to 100 GHz) for use in missile radomes usable in systems specified in 1.A. or 19.A.1. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,654 | Bulk machinable silicon-carbide reinforced unfired ceramic usable for nose tips usable in systems specified in 1.A. or 19.A.1. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,655 | Reinforced silicon-carbide ceramic composites usable for nose tips, re-entry vehicles, nozzle flaps, usable in systems specified in 1.A. or 19.A.1. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,656 | 6.C.7. Tungsten, molybdenum, and alloys of these metals in the form of uniform spherical or atomised particles of 500 x 10-6 m (500 µm) diameter or less with a purity of 97% or higher for fabrication of rocket motor components, i.e. heat shields, nozzle substrates, nozzle throats, and thrust vector control surfaces, usable in systems specified in 1.A. or 19.A.1. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,657 | 6.C.8. Maraging steels having an ultimate tensile strength equal to or greater than 1.5 GPa, measured at 20oC, in the form of sheet, plate or tubing with a wall or plate thickness equal to or less than 5.0 mm usable in systems specified in 1.A. or 19.A.1. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,658 | Maraging steels are iron alloys generally characterised by high nickel, very low carbon content and use substitutional elements or precipitates to produce strengthening and age-hardening of the alloy. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,659 | 6.C.9. Titanium-stabilized duplex stainless steel (Ti-DSS) usable in the systems specified in 1.A. or 19.A.1. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,660 | Containing 17.0 - 23.0 weight percent chromium and 4.5 - 7. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,661 | Having a titanium content of greater than 0. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,662 | Tubes having an outer diameter of 600 mm or more and a wall thickness of 3 mm or less. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,663 | 6.D.1. "Software" specially designed or modified for the "use" of equipment specified in 6.B.1. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,664 | 6.D.2. "Software" specially designed or modified for the equipment specified in 6.B.3., 6.B.4. or 6.B.5. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,665 | 6.E.1. "Technology", in accordance with the General Technology Note, for the "development", "production" or "use" of equipment, materials or "software" specified in 6.A., 6.B., 6.C. or 6.D. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,666 | 6.E.2. "Technical data" (including processing conditions) and procedures for the regulation of temperature, pressures or atmosphere in autoclaves or hydroclaves when used for the production of composites or partially processed composites, usable for equipment or materials specified in 6.A. or 6.C. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,667 | 6.E.3. "Technology" for producing pyrolytically derived materials formed on a mould, mandrel or other substrate from precursor gases which decompose in the 1,300oC to 2,900oC temperature range at pressures of 130 Pa (1 mm Hg) to 20 kPa (150 mm Hg) including "technology" for the composition of precursor gases, flow-rates, and process control schedules and parameters. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,668 | 9.A.1. Integrated flight instrument systems which include gyrostabilisers or automatic pilots, designed or modified for use in the systems specified in 1.A., or 19.A.1. or 19.A.2. and specially designed components therefor. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,669 | 9.A.2. Gyro-astro compasses and other devices which derive position or orientation by means of automatically tracking celestial bodies or satellites, and specially designed components therefor. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,670 | 9.A.3. Linear accelerometers, designed for use in inertial navigation systems or in guidance systems of all types, usable in the systems specified in 1.A., 19.A.1. or 19.A.2. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,671 | b. 'Bias' 'repeatability' less (better) than 1250 micro g. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,672 | 'Bias' is defined as the accelerometer output when no acceleration is applied. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,673 | 'Scale factor' is defined as the ratio of change in output to a change in the input. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,674 | The measurement of 'bias' and 'scale factor' refers to one sigma standard deviation with respect to a fixed calibration over a period of one year. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,675 | 'The closeness of agreement among repeated measurements of the same variable under the same operating conditions when changes in conditions or non-operating periods occur between measurements'. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,676 | Item 9.A.3. does not control accelerometers specially designed and developed as Measurement While Drilling (MWD) sensors for use in downhole well service operations. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,677 | 9.A.4. All types of gyros usable in the systems specified in 1.A., 19.A.1 or 19.A.2., with a rated 'drift rate' 'stability' of less than 0.5 degrees (1 sigma or rms) per hour in a 1 g environment, and specially designed components therefor. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,678 | 'Drift rate' is defined as the component of gyro output that is functionally independent of input rotation and is expressed as an angular rate. IEEE STD 528-2001 paragraph 2. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,679 | 'Stability' is defined as a measure of the ability of a specific mechanism or performance coefficient to remain invariant when continuously exposed to a fixed operating condition. (This definition does not refer to dynamic or servo stability.) (IEEE STD 528-2001 paragraph 2. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,680 | 9.A.5. Accelerometers or gyros of any type, designed for use in inertial navigation systems or in guidance systems of all types, specified to function at acceleration levels greater than 100 g, and specially designed components therefor. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,681 | vibration or shock. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,682 | 9.A.6. Inertial or other equipment using accelerometers specified in 9.A.3. or 9.A.5. or gyros specified in 9.A.4. or 9.A.5., and systems incorporating such equipment, and specially designed components therefor. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,683 | 9.A.7. 'Integrated navigation systems', designed or modified for the systems specified in 1.A., 19.A.1. or 19.A.2. and capable of providing a navigational accuracy of 200 m CEP or less. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,684 | An inertial measurement device e.g. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,685 | One or more external sensors used to update the position and/or velocity, either periodically or continuously throughout the flight e.g. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,686 | c. Integration hardware and software. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,687 | N.B. For integration "software", see Item 9.D.4. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,688 | a. Internal tilt compensation in pitch (+/- 90 degrees) and having roll (+/- 180 degrees) axes. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,689 | b. Capable of providing azimuthal accuracy better (less) than 0. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,690 | c. Designed or modified to be integrated with flight control and navigation systems. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,691 | Flight control and navigation systems in Item 9.A.8. include gyrostabilisers, automatic pilots and inertial navigation systems. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,692 | 9.B.1. "Production equipment", and other test, calibration and alignment equipment, other than that described in 9.B.2., designed or modified to be used with equipment specified in 9.A. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,693 | Equipment specified in 9.B.1. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,694 | Accelerometer Test Station. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,695 | Capable of balancing to a residual specific unbalance of 0. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,696 | b. Indicator heads (sometimes known as balancing instrumentation) designed or modified for use with machines specified in 9.B.2.a. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,697 | A rate resolution equal to or less than 6 degrees/s and an accuracy equal to or less than 0. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,698 | b. Having a worst-case rate stability equal to or better (less) than plus or minus 0. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,699 | e. Centrifuges capable of imparting accelerations above 100 g and designed or modified to incorporate sliprings or integrated non-contact devices capable of transferring electrical power, signal information, or both. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,700 | The only balancing machines, indicator heads, motion simulators, rate tables, positioning tables and centrifuges specified in Item 9 are those specified in 9.B.2. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,701 | 9.B.2.a. does not control balancing machines designed or modified for dental or other medical equipment. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,702 | 9.B.2.c. and 9.B.2.d. do not control rotary tables designed or modified for machine tools or for medical equipment. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,703 | Rate tables not controlled by 9.B.2.c. and providing the characteristics of a positioning table are to be evaluated according to 9.B.2.d. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,704 | Equipment that has the characteristics specified in 9.B.2.d. which also meets the characteristics of 9.B.2.c. will be treated as equipment specified in 9.B.2.c. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,705 | Item 9.B.2.c. applies whether or not sliprings or integrated non-contact devices are fitted at the time of export. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,706 | Item 9.B.2.e. applies whether or not sliprings or integrated non-contact devices are fitted at the time of export. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,707 | 9.D.1. "Software" specially designed or modified for the "use" of equipment specified in 9.A. or 9.B. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,708 | 9.D.2. Integration "software" for the equipment specified in 9.A.1. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,709 | 9.D.3. Integration "software" specially designed for the equipment specified in 9.A.6. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,710 | systems' specified in 9.A.7. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,711 | A common form of integration "software" employs Kalman filtering. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,712 | 9.E.1. "Technology", in accordance with the General Technology Note, for the "development", "production" or "use" of equipment or "software" specified in 9.A., 9.B. or 9.D. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,713 | Equipment or "software" specified in 9.A. or 9.D. may be exported as part of a manned aircraft, satellite, land vehicle, marine/submarine vessel or geophysical survey equipment or in quantities appropriate for replacement parts for such applications. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,714 | 10.A.1. Hydraulic, mechanical, electro-optical, or electromechanical flight control systems (including fly-by-wire systems) designed or modified for the systems specified in 1.A. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,715 | 10.A.2. Attitude control equipment designed or modified for the systems specified in 1.A. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,716 | 10.A.3. Flight control servo valves designed or modified for the systems in 10.A.1. or 10.A.2., and designed or modified to operate in a vibration environment greater than 10 g rms between 20 Hz and 2 kHz. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,717 | Systems, equipment or valves specified in 10.A. may be exported as part of a manned aircraft or satellite or in quantities appropriate for replacement parts for manned aircraft. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,718 | 10.B.1. Test, calibration, and alignment equipment specially designed for equipment specified in 10.A. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,719 | 10.D.1. "Software" specially designed or modified for the "use" of equipment specified in 10.A. or 10.B. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,720 | "Software" specified in 10.D.1. may be exported as part of a manned aircraft or satellite or in quantities appropriate for replacement parts for manned aircraft. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,721 | 10.E.1. Design "technology" for integration of air vehicle fuselage, propulsion system and lifting control surfaces, designed or modified for the systems specified in 1.A. or 19.A.2., to optimise aerodynamic performance throughout the flight regime of an unmanned aerial vehicle. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,722 | 10.E.2. Design "technology" for integration of the flight control, guidance, and propulsion data into a flight management system, designed or modified for the systems specified in 1.A. or 19.A.1., for optimisation of rocket system trajectory. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,723 | 10.E.3. "Technology", in accordance with the General Technology Note, for the "development", "production" or "use" of equipment or "software" specified in 10.A., 10.B. or 10.D. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,724 | 11.A.1. Radar and laser radar systems, including altimeters, designed or modified for use in the systems specified in 1.A. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,725 | Laser radar systems embody specialised transmission, scanning, receiving and signal processing techniques for utilisation of lasers for echo ranging, direction finding and discrimination of targets by location, radial speed and body reflection characteristics. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,726 | 11.A.2. Passive sensors for determining bearings to specific electromagnetic sources (direction finding equipment) or terrain characteristics, designed or modified for use in the systems specified in 1.A. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,727 | 11.A.3. Receiving equipment for Global Navigation Satellite Systems GNSS; e.g. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,728 | a. Designed or modified for use in systems specified in 1.A. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,729 | Being specially designed to employ anti-jam features (e.g. null steering antenna or electronically steerable antenna) to function in an environment of active or passive countermeasures. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,730 | 11.A.3.b.2. and 11.A.3.b.3. do not control equipment designed for commercial, civil or 'Safety of Life' (e.g. data integrity, flight safety) GNSS services. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,731 | 11.A.4. Electronic assemblies and components, designed or modified for use in the systems specified in 1.A. or 19.A. and specially designed for military use and operation at temperatures in excess of 125oC. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,732 | Equipment specified in 11.A. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,733 | e. Imaging sensor equipment (both active and passive). |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,734 | Equipment specified in 11.A. may be exported as part of a manned aircraft or satellite or in quantities appropriate for replacement parts for manned aircraft. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,735 | 11.D.1. "Software" specially designed or modified for the "use" of equipment specified in 11.A.1., 11.A.2. or 11.A.4. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,736 | 11.D.2. "Software" specially designed for the "use" of equipment specified in 11.A.3. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,737 | c. Design "technology" for determination of hardening criteria for the above. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,738 | 11.E.2. "Technology", in accordance with the General Technology Note, for the "development", "production" or "use" of equipment or "software" specified in 11.A. or 11.D. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,739 | 12.A.1. Apparatus and devices, designed or modified for the handling, control, activation and launching of the systems specified in 1.A., 19.A.1., or 19.A.2. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,740 | 12.A.2. Vehicles designed or modified for the transport, handling, control, activation and launching of the systems specified in 1.A. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,741 | 12.A.3. Gravity meters (gravimeters), gravity gradiometers, and specially designed components therefor, designed or modified for airborne or marine use, and having a static or operational accuracy of 7 x 10-6 m/s2 (0.7 milligal) or better, with a time to steady-state registration of two minutes or less, usable for systems specified in 1.A. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,742 | 12.A.4. Telemetry and telecontrol equipment, including ground equipment, designed or modified for systems specified in 1.A., 19.A.1. or 19.A.2. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,743 | 12.A.4. does not control equipment designed or modified for manned aircraft or satellites. |
144 | DAC-NLS. CertainMissileTechItems.2009-10-12.af.txt | 9,744 | 12.A.4. does not control ground based equipment designed or modified for terrestrial or marine applications. |
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