 Provides:
- search, lock-on and tracking of moving targets upon target designation from the missile inertial navigation system:
- 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 followed with active homing at final part of flight.
Specifications:
1. Composition:
- controlled coordinator with antenna;
- transmitting channel hardware;
- receiving channel hardware;
- on-board digital computing system.
2. Type of guidance system:
inertial guidance with updating and active homing;
3. Uplink and ARS provide missile RVV-AE launch from an aircraft of MIG-29 type in front hemisphere at maximum range of up to 80 km;
4. Time ready after preliminary warm-up for 2 min : 1.0 sec, no more;
5. Mass (less radome) : 16 kg, no more;
6. Diameter : 200 mm;
7. Length (less radome) : 604 mm. Collaboration is possible on the basis of purchasing and testing RVV-AE missile.
ARS parameters may be changed upon Customer’s will.
Collaboration supposes purchase and tests of the missile RVV-AE.
According to the customer"s desire parameters of the seeker can be changed.
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