
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 | ||
