 Purpose: to fit air-to-air and surface-to-air missiles.
Provides: - search, lock-on and tracking of moving targets upon target designation from airborne and air defense radars: -measuring of target angular coordinates, angular rates and missile-to-target closing speed; - generation and transfer of signals measured to missile control system. Operating modes: - active (“fire-and-forget”) completely autonomous mode using only preliminary target designation data, without any external radar support during flight; - inertial guidance with updating.
Specifications: 1. Composition: - controlled coordinator with antenna; - transmitting channel hardware; - receiving channel hardware; - reprogrammed on-board digital computing system in composition of control computer and signal processor. 2. Type of guidance system: - inertial guidance with updating and active homing; 3. Lock-on range of targets with RCS = 5m2 : 25 km, no less; 4. Speed of on-board digital computing system : 50106 op/s, no less; 5. Time ready (after preliminary warm-up for 2 min) : 1.0 sec; 6. Mass (less radome) : 10 kg, no more; 7. Diameter : 200 mm; 8. Length (less radome) : 400 mm. Collaboration supposes initiation of ordered or joint R-effort on the basis of Advanced seeker 9B-1103M with follow-on as R&D efforts.
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