| Specifications |
| Contractor |
|
| Initial operational capability | 1956
|
| Production terminated | 1960
|
| First detected | 1961
|
| Guidance system | K-III receiver, Kometa-M PARGSN K-II, APK-5V autopilot, altimeter
|
| Engine | Turbojet engine RD-500K, thrust 1500 kgf
|
| warhead | Armor-piercing , 1015 kg
|
| Launch range | 80–140 km
|
| Speed | 1150 km/h
|
| Flight altitude | 4000–400 m, dive in the final section
|
| Launch altitude | 2000–4000 m
|
| Accuracy | 81% hit chance (60% in interference)
|
| Starting weight | 2850 kg
|
| Length | 8.29 m
|
| Hull diameter | 1.12 m
|
| Wingspan | 4.722 m
|
| Wing area | 8.5 m2
|
