| 10Kh | |
|---|---|
| Type | cruise missile |
| Place of origin | USSR |
| Production history | |
| Designer | Vladimir N. Chelomey |
| Designed | 1945 |
| Manufacturer | OKB-52 |
| Produced | 1945 |
| No. built | 300 (10Kh) |
| Variants | 10Kh Izdeliye 30 10KhN 14Kh 14KhK1 15Kh 16Kh 17Kh 18Kh Gliding bomb |
| Specifications | |
| Engine | Chelomey D-3 ca 3.924 kN (882 lbf) thrust |
| Propellant | Gasoline |
Operational range | 260 - 300 km |
| Boost time | Solid fuel rockets (ramp launching) |
Launch platform | Petlyakov Pe-8 Tupolev Tu-2LL |
10Kh was the designation for the initial series of Soviet Union pulse jet engine powered air-launched cruise missiles, reverse engineered from the Fieseler Fi 103 (V-1) flying bomb, developed in the 1950s by OKB-52 under the leadership of Vladimir Nikolaevič Čelomej (Chelomey) and cancelled in the same decade.[1][2]
- ^ "Russia: VPK NPO Mashinostroyeniya". 2008. Archived from the original on January 13, 2010. Retrieved March 3, 2010.
- ^ Zak, Anatoly (2008). "ROCKETS: Cruise missiles". Retrieved March 3, 2010.
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