RD-0105
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Credit: KBKhA
Kosberg LOx/Kerosene rocket engine. Luna 8K72, Vostok 8K72 upper stage. Out of production. Developed jointly with OKB-1 in nine months on the basis of OKB-1's steering chamber from the RD-107 engine. First flight 1958.
Engine: 125 kg (275 lb). Chamber Pressure: 45.00 bar. Thrust to Weight Ratio: 40.
Related
- Country
- Russia
- Launch Vehicles
- Vostok 8K72, Vostok-L 8K72
- Propellants
- Lox/Kerosene
- Stages
- Luna 8K72-2, Vostok 8K72-2
- Agency
- Kosberg bureau