RD-108-11D512
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 11A511-1, Soyuz 11A511U-1. Design 2000. Diameter is per chamber. First flight 1965.
Chambers: 4. Thrust (sl): 746.400 kN (167,797 lbf). Thrust (sl): 76,100 kgf. Engine: 1,400 kg (3,000 lb). Chamber Pressure: 51.00 bar. Thrust to Weight Ratio: 72.59.
Related
- Country
- Russia
- Launch Vehicles
- Soyuz 11A511, Soyuz-U
- Propellants
- Lox/Kerosene
- Stages
- Soyuz 11A511-1, Soyuz 11A511U-1
- Agency
- Glushko bureau
Photo Gallery
RD-107
Credit: © Mark Wade
