RD-108-8D75K
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. Molniya 8K78-1, R-7A 8K74-1, Voskhod 11A57-1, Vostok 8A92-1, Vostok 8A92M-1. Diameter is per chamber. First flight 1959.
Chambers: 4. Thrust (sl): 740.400 kN (166,449 lbf). Thrust (sl): 75,504 kgf. Engine: 1,252 kg (2,760 lb). Chamber Pressure: 51.00 bar. Area Ratio: 18.9. Thrust to Weight Ratio: 76.59.
Related
- Country
- Russia
- Launch Vehicles
- R-7A, Molniya 8K78, Voskhod 11A57, Vostok 8A92, Sputnik 11A59, Vostok 8A92M
- Propellants
- Lox/Kerosene
- Agency
- Glushko bureau
Photo Gallery
RD-107
Credit: © Mark Wade
