| name | image | Detonation | guidance system | type | warhead | date designed | date end service | date start service | Diameter (m) | Engine | country of origin | continent of origin | launchpad | Length (m) | mass (kg) | Number built | Operational range (m) | Speed (m/s) | Wingspan (m) |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 2K11 Krug |  | Late 1965 | 1965 | 1 | V59 V-12 water-cooled diesel$#$520 hp | 9 | 28,200 | ||||||||||||
| 3M-54 Kalibr |  | Multi-stage [Multi-stage] Solid-Fuel [Solid-fuel_rocket] rocket, Turbojet [Turbojet] engine for 3M-54/E/TE/E1/TE1, -14/E/TE, Solid fuel rocket for 91RE1/RTE2 | Russia | Europe | |||||||||||||||
| 3M6 Shmel |  | 1959 | 24 | 1,955 | |||||||||||||||
| 3M7 | dwustopniowy silnik rakietowy na staly material pedny | 1 | 50 | ||||||||||||||||
| A-135 anti-ballistic missile system |  | 33,000 |