Specifications | ||
Contractor | Chelomey | |
Entered Service | 1969 | |
Total length | 8.84 meters | |
Diameter | ||
Wingspan | ||
Weight | 3,000 kg | |
Warhead | ||
Propulsion | solid-fuel booster and sustainer [liquid-fuel rocket engine according to some sources] | |
Maximum Speed | Mach 0.8 [Mach 1.4 according to some sources] | |
Maximum effective range | 110 km | |
Guidance mode | inertial terminal homing | |
Single-shot hit probability |