| FEATURES | combined guidance system management system (INS) with radio and midcourse radar homing in the final phase of flight
|
| Controls | aerodynamic rudders
|
| Firing range, km | 300-400
|
| Target speed, km / h | 4000
|
| Average missile speed, m / s | 1400
|
| Target hitting altitude, m | 3000-30000 Target
|
| overload, units | 12
|
| warhead | High-explosive fragmentation
|
| Number of stages | 2
|
| Missile length, mm: - full | 7400
|
| without launch stage | 5800 - 6000
|
| Max. body diameter, mm | 400
|
| Max. diameter of the starting stage, mm | 510
|
| Starting weight, kg | 700 - 750
|
| Type of rocket engine | 3L10 solid propellant
|
| length, mm | 1400
|
