RD-107-8D74-1958
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Credit: © Mark Wade
Glushko LOx/Kerosene rocket engine. Luna 8K72-0. Out of production. Diameter is per chamber. First flight 1958.
Chambers: 4. Thrust (sl): 806.400 kN (181,286 lbf). Thrust (sl): 82,224 kgf. Engine: 1,155 kg (2,546 lb). Chamber Pressure: 58.40 bar. Area Ratio: 18.9. Thrust to Weight Ratio: 87.44. Oxidizer to Fuel Ratio: 2.47.
Related
- Country
- Russia
- Launch Vehicles
- Vostok-L 8K72
- Propellants
- Lox/Kerosene
- Stages
- Luna 8K72-0
- Agency
- Glushko bureau
Photo Gallery
R-7 aft end
Credit: © Mark Wade
