RD-107-11D511
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. Soyuz 11A511-0, Soyuz 11A511U-0. Design 2000. Diameter is per chamber. First flight 1965.
Chambers: 4. Thrust (sl): 821.600 kN (184,703 lbf). Thrust (sl): 83,800 kgf. Engine: 1,200 kg (2,600 lb). Chamber Pressure: 58.50 bar. Thrust to Weight Ratio: 84.27. Oxidizer to Fuel Ratio: 2.47.
Related
- Country
- Russia
- Launch Vehicles
- Soyuz 11A511, Soyuz-U
- Propellants
- Lox/Kerosene
- Stages
- Soyuz 11A511-0, Soyuz 11A511U-0
- Agency
- Glushko bureau
Photo Gallery
R-7 aft end
Credit: © Mark Wade
