6A108

Radar and laser radar systems designed or modified for use in space launch vehicles specified in 9A004 or sounding rockets specified in 9A104;

Precision tracking systems, usable for ‘missiles’, as follows:

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;

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;

Radomes designed to withstand a combined thermal shock greater than 4,184 × 10^6 J/m^2 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).