7A117 | "Guidance sets", usable in "missiles" 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 "guidance sets" designed for missiles with a range under 300 km or manned aircraft . |
7B001 | Test, calibration or alignment equipment specially designed for equipment specified in 7A117 above .
Note: 7B001 does not control test, calibration or alignment equipment for Maintenance Level I or Maintenance Level II. |
7B003 | Equipment specially designed for the "production" of equipment specified in 7A117 above . |
7B103 | "Production facilities" specially designed for equipment specified in 7A117 above . |
7D101 | "Software" specially designed for the "use" of equipment specified in 7B003 or 7B103 above . |
7E001 | "Technology" according to the General Technology Note for the "development" of equipment or "software" specified in 7A117, 7B003, 7B103 or 7D101 above . |
7E002 | "Technology" according to the General Technology Note for the "production" of equipment specified in 7A117, 7B003 and 7B103 above . |
7E101 | "Technology" according to the General Technology Note for the "use" of equipment specified in 7A117, 7B003, 7B103 and 7D101 above . |
9A004 | Space launch vehicles capable of delivering at least a 500 kg payload to a range of at least 300 km .
N.B. SEE ALSO 9A104. Note 1: 9A004 does not control payloads. |
9A005 | Liquid rocket propulsion systems containing any of the systems or components specified in 9A006 usable for space launch vehicles specified in 9A004 above or sounding rockets specified in 9A104 below .
N.B. SEE ALSO 9A105 and 9A119. |
9A007.a. | Solid rocket propulsion systems, usable for space launch vehicles specified in 9A004 above or sounding rockets specified in 9A104 below , with any of the following:
N.B. SEE ALSO 9A119. a. Total impulse capacity exceeding 1,1 MNs;
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9A008.d. | Components, as follows, specially designed for solid rocket propulsion systems:
N.B. SEE ALSO 9A108.c. d. Movable nozzle or secondary fluid injection thrust vector control systems, usable for space launch vehicles specified in 9A004 above or sounding rockets specified in 9A104 below , capable of any of the following:
1. Omni-axial movement exceeding ± 5 o ;
2. Angular vector rotations of 20 o /s or more; or
3. Angular vector accelerations of 40 o /s 2 or more.
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9A104 | Sounding rockets, capable of delivering at least a 500 kg payload to a range of at least 300 km.
N.B. SEE ALSO 9A004. |
9A105.a. | Liquid propellant rocket engines, as follows:
N.B. SEE ALSO 9A119. a. Liquid propellant rocket engines usable in ‘missiles’, other than those specified in 9A005, integrated, or designed or modified to be integrated, into a liquid propellant propulsion system which has a total impulse capacity equal to or greater than 1,1 MNs having a total impulse capacity equal to or greater than 1,1 MNs; except liquid propellant apogee engines designed or modified for satellite applications and having all of the following :
1. nozzle throat diameter of 20 mm or less; and
2. combustion chamber pressure of 15 bar or less.
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9A106.c. | Systems or components, other than those specified in 9A006, usable in "missiles", as follows, specially designed for liquid rocket propulsion systems:
c. Thrust vector control sub-systems, except those designed for rocket systems that are not capable of delivering at least a 500 kg payload to a range of at least 300 km .
Technical Note: Examples of methods of achieving thrust vector control specified in 9A106.c. are:
2. Fluid or secondary gas injection;
3. Movable engine or nozzle;
4. Deflection of exhaust gas stream (jet vanes or probes); or
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9A108.c. | Components, other than those specified in 9A008, usable in ‘ missiles ’ as follows, specially designed for solid rocket propulsion systems:
c. Thrust vector control sub-systems, except those designed for rocket systems that are not capable of delivering at least a 500 kg payload to a range of at least 300 km .
Technical Note: Examples of methods of achieving thrust vector control specified in 9A108.c. are:
2. Fluid or secondary gas injection;
3. Movable engine or nozzle;
4. Deflection of exhaust gas stream (jet vanes or probes); or
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9A116 | Reentry vehicles, usable in "missiles", and equipment designed or modified therefor, as follows, except for reentry vehicles designed for non-weapon payloads :
b. Heat shields and components therefor fabricated of ceramic or ablative materials;
c. Heat sinks and components therefor fabricated of light-weight, high heat capacity materials;
d. Electronic equipment specially designed for reentry vehicles.
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9A119 | Individual rocket stages, usable in complete rocket systems or unmanned aerial vehicles, capable of delivering at least a 500 kg payload to a range of 300 km, other than those specified in 9A005 or 9A007.a. above |
9B115 | Specially designed "production equipment" for the systems, sub-systems and components specified in 9A005, 9A007.a., 9A008.d., 9A105.a., 9A106.c., 9A108.c., 9A116 or 9A119 above . |
9B116 | Specially designed "production facilities" for the space launch vehicles specified in 9A004, or systems, sub-systems, and components specified in 9A005, 9A007.a., 9A008.d., 9A104, 9A105.a., 9A106.c., 9A108.c., 9A116 or 9A119 above . |
9D101 | ‘Software’ specially designed for the ‘use’ of goods specified in 9B116 above . |
9E001 | "Technology" according to the General Technology Note for the "development" of equipment or "software" specified in 9A004, 9A005, 9A007.a., 9A008.d., 9B115, 9B116 or 9D101 above . |
9E002 | "Technology" according to the General Technology Note for the "production" of equipment specified in 9A004, 9A005, 9A007.a., 9A008.d., 9B115 or 9B116 above .
Note: For "technology" for the repair of controlled structures, laminates or materials, see 1E002.f. |
9E101 | "Technology" according to the General Technology Note for the "development" or "production" of goods specified in 9A104, 9A105.a., 9A106.c., 9A108.c., 9A116 or 9A119 above . |
9E102 | "Technology" according to the General Technology Note for the "use" of space launch vehicles specified in 9A004, 9A005, 9A007.a., 9A008.d., 9A104, 9A105.a., 9A106.c., 9A108.c., 9A116, 9A119, 9B115, 9B116 or 9D101 above . |