- List
- EU dual-use list – Annex I to Regulation (EU) 2021/821, updated annually
- Originating regime
- MTCR
a. Radar and laser radar systems designed or modified for use in space launch vehicles specified in 9A004 or sounding rockets specified in 9A104;
Note:
6A108.a. includes the following:
a. Terrain contour mapping equipment;
b. Scene mapping and correlation (both digital and analogue) equipment;
c. Doppler navigation radar equipment;
d. Passive interferometer equipment;
e. Imaging sensor equipment (both active and passive).
b. Precision tracking systems, usable for 'missiles', as follows:
1. Tracking systems which use a code translator in conjunction with either surface or airborne references or navigation satellite systems to provide real-time measurements of in-flight position and velocity;
2. Range instrumentation radars including associated optical/infrared trackers with all of the following capabilities:
a. Angular resolution better than 1,5 milliradians;
b. Range of 30 km or greater with a range resolution better than 10 m rms; and
c. Velocity resolution better than 3 m/s;
Technical Note:
In 6A108.b. 'missile' means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
c. Radomes designed to withstand a combined thermal shock greater than 4,184 × 106 J/m2 accompained by a peak over pressure of greater than 50 kPa, and usable in "missiles" for protecting against nuclear effects (e.g. electromagnetic pulse (EMP), X-rays, combined blast and thermal effects).
Note:
6A108.a. includes the following:
a. Terrain contour mapping equipment;
b. Scene mapping and correlation (both digital and analogue) equipment;
c. Doppler navigation radar equipment;
d. Passive interferometer equipment;
e. Imaging sensor equipment (both active and passive).
b. Precision tracking systems, usable for 'missiles', as follows:
1. Tracking systems which use a code translator in conjunction with either surface or airborne references or navigation satellite systems to provide real-time measurements of in-flight position and velocity;
2. Range instrumentation radars including associated optical/infrared trackers with all of the following capabilities:
a. Angular resolution better than 1,5 milliradians;
b. Range of 30 km or greater with a range resolution better than 10 m rms; and
c. Velocity resolution better than 3 m/s;
Technical Note:
In 6A108.b. 'missile' means complete rocket systems and unmanned aerial vehicle systems capable of a range exceeding 300 km.
c. Radomes designed to withstand a combined thermal shock greater than 4,184 × 106 J/m2 accompained by a peak over pressure of greater than 50 kPa, and usable in "missiles" for protecting against nuclear effects (e.g. electromagnetic pulse (EMP), X-rays, combined blast and thermal effects).