SPECIFIC FEATURES
RVV-BD guided missile specific features: -
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the missile is equipped with the combined control system ensuring inertial radio-correction guidance at the major flight section and radar homing at the end flight path section.
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the double-thrust solid-fuel engine with internal start when the missile is separated from the carrier aircraft;
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the missile has digital active radar homing head allowing for the “fire-and-forget” firing.
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PURPOSE AND MAIN TASKS
RVV-BD long-range aircraft guided air-to-air missile is designed for hitting the air-borne targets (fighters, attack aircraft, bombers, military carrier aircraft, helicopters, cruise missiles) day-and-night, at any angles under electronic countermeasures conditions against the earth and water surface background, inclusive of the multiple target “fire-and-forget” firing.
Main Performance Specifications
Launch weight, kg |
510 |
Warhead weight |
60 |
Hit target altitude, km |
0.015...25 |
Maximum hit target speed, km/h |
2 500 |
Maximum hit target acceleration, g |
8 |
Launch range, maximum to the FA, km |
up to 200 |
Operating range of the acting MRV for the fighter aircraft, km:
maximum (FA)
minimum (RA) |
30
10 |
Warhead |
fragmentation - high-explosive |
Probability of fighter-type target hitting with one missile |
0.6...0.8 |
Guidance system
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Inertial with radio-correction + active radar
homing |
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