| No | Relevant item(s) from Annex to Regulation (EC) No 1183/2007 | Description |
|---|
| I.7A.001 | ex 7A002*
( ex 7A002.a and ex 7A002.d)
| Gyros having any of the following characteristics, and specially designed components therefor:
N.B.: See also I.7A.003.
a. A ‘ drift rate ’ ‘ stability ’ , when measured in a 1 g environment over a period of one month and with respect to a fixed calibration value, of less (better) than 0,5 degree per hour when specified to function at linear acceleration levels up to and including 100 g; or
b. Specified to function at linear acceleration levels exceeding 100 g.
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| I.7A.002 | 7A101, ex 7A001.a.3 | Accelerometers as follows, and specially designed components therefor:
a. Linear accelerometers, designed for use in inertial navigation systems or in guidance systems of all types, usable in ‘ missiles ’ , having all the following characteristics, and specially designed components therefor;
1. A ‘ bias ’ ‘ repeatability ’ of less (better) than 1 250 micro g; and
2. A ‘ scale factor ’ ‘ repeatability ’ of less (better) than 1 250 ppm;
Note: I.7A.002.a. does not specify accelerometers which are specially designed and developed as MWD (Measurement While Drilling) Sensors for use in downhole well service operations.
Technical Notes: 1. In I.7A.002.a. ‘ missile ’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km; 2. In I.7A.002.a. the measurement of ‘ bias ’ and ‘ scale factor ’ refers to a one sigma standard deviation with respect to a fixed calibration over a period of one year; b. Continuous output accelerometers specified to function at acceleration levels exceeding 100 g.
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| I.7A.003 | 7A102* | All types of gyros, other than those specified in I.7A.001, usable in ‘ missiles ’ , with a rated ‘ drift rate ’ ‘ stability ’ of less than 0,5° (1 sigma or rms) per hour in a 1 g environment and specially designed components therefor.
Technical Note: In I.7A.003 ‘ missile ’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
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| I.7A.004 | ex 7A103
(7A103.a, ex 7A103.b and 7A103.c)
| Instrumentation, navigation equipment and systems, as follows; and specially designed components therefor:
Inertial or other equipment using accelerometers specified in I.7A.002 or gyros specified in I.7A.001 or I.7A.003 and systems incorporating such equipment;
Integrated flight instrument systems, which include gyrostabilisers or automatic pilots, designed or modified for use in ‘ missiles ’ ;
‘ Integrated navigation systems ’ , designed or modified for ‘ missiles ’ and capable of providing a navigational accuracy of 200 m Circle of Equal Probability (CEP) or less.
Technical Notes: 1. An ‘ integrated navigation system ’ typically incorporates the following components: a. An inertial measurement device (e.g., an attitude and heading reference system, inertial reference unit, or inertial navigation system);
b. One or more external sensors used to update the position and/or velocity, either periodically or continuously throughout the flight (e.g., satellite navigation receiver, radar altimeter, and/or Doppler radar); and
c. Integration hardware and software;
2. In I.7A.004.c. ‘ missile ’ means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
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| I.7A.005 | 7A104 | 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. |
| I.7A.006 | 7A105 | Receiving equipment for Global Navigation Satellite Systems (GNSS; e.g. GPS, GLONASS, or Galileo), having any of the following characteristics, and specially designed components therefor:
a. Designed or modified for use in space launch vehicles specified in I.9A.001, unmanned aerial vehicles specified in I.9A.003 or sounding rockets specified in I.9A.005; or
N.B.: See also Military Goods Controls for receiving equipment for rockets or missiles.
b. Designed or modified for airborne applications and having any of the following:
1. Capable of providing navigation information at speeds in excess of 600 m/s;
2. Employing decryption, designed or modified for military or governmental services, to gain access to GNSS secured signal/data; or
3. 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.
Note: I.7A.006.b.2. and I.7A.006.b.3. do not prohibit equipment designed for commercial, civil or ‘Safety of Life’ (e.g., data integrity, flight safety) GNSS services
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| I.7A.007 | 7A106 | Altimeters of radar or laser radar type, designed or modified for use in space launch vehicles specified in I.9A.001 or sounding rockets specified in I.9A.005.
N.B.: See also Military Goods Controls for altimeters for rockets or missiles.
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| I.7A.008 | 7A115 | Passive sensors for determining bearing to specific electromagnetic source (direction finding equipment) or terrain characteristics, designed or modified for use in space launch vehicles specified in I.9A.001 or sounding rockets specified in I.9A.005.
N.B.: See also Military Goods Controls for passive sensors for rockets or missiles.
Note: I.7A.008 includes sensors for the following equipment:
a. Terrain contour mapping equipment;
b. Imaging sensor equipment (both active and passive);
c. Passive interferometer equipment.
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| I.7A.009 | 7A116 | Flight control systems and servo valves, as follows; designed or modified for use in space launch vehicles specified in I.9A.001 or sounding rockets specified in I.9A.005.
N.B.: See also Military Goods Controls for flight control systems and servo valves for rockets or missiles.
a. Hydraulic, mechanical, electro-optical, or electro-mechanical flight control systems (including fly-by-wire types);
b. Attitude control equipment;
c. Flight control servo valves designed or modified for the systems specified in I.7A.009.a. or I.7A.009.b., and designed or modified to operate in a vibration environment greater than 10 g rms between 20 Hz and 2 kHz.
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| I.7A.010 | 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). |
| I.7A.011 | 7B001 | Test, calibration or alignment equipment specially designed for equipment specified in I.7A.001 to I.7A.010. |
| I.7A.012 | 7B002 | Equipment, as follows, specially designed to characterize mirrors for ring ‘ laser ’ gyros:
N.B.: See also I.7A.014.
a. Scatterometers having a measurement accuracy of 10 ppm or less (better);
b. Profilometers having a measurement accuracy of 0,5 nm (5 angstrom) or less (better).
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| I.7A.013 | 7B003* | Equipment specially designed for the ‘ production ’ of equipment specified in I.7A.001 to I.7A.010.
Note: I.7A.013 includes:
a. Gyro tuning test stations;
b. Gyro dynamic balance stations;
c. Gyro run-in/motor test stations;
d. Gyro evacuation and fill stations;
e. Centrifuge fixtures for gyro bearings;
f. Accelerometer axis align stations;
h. Accelerometer test stations;
i. Inertial measurement unit (IMU) module testers;
j. Inertial measurement unit (IMU) platform testers;
k. Inertial measurement unit (IMU) stable element handling fixtures;
l. Inertial measurement unit (IMU) platform balance fixture.
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| I.7A.014 | 7B102 | Reflectometers specially designed to characterise mirrors, for ‘ laser ’ gyros, having a measurement accuracy of 50 ppm or less (better). |
| I.7A.015 | 7B103 | ‘ Production facilities ’ and ‘ production equipment ’ as follows:
a. ‘ Production facilities ’ specially designed for equipment specified in I.7A.010;
b. ‘ Production equipment ’ , and other test, calibration and alignment equipment, other than that specified in I.7A.011 to I.7A.013, designed or modified to be used with equipment specified in I.7A.001 to I.7A.010.
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