RD-108-8D75PS
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. Sputnik 8K71PS-1. Out of Production. Diameter is per chamber. First flight 1957.
Chambers: 4. Thrust (sl): 713.600 kN (160,424 lbf). Thrust (sl): 72,768 kgf. Engine: 1,250 kg (2,750 lb). Chamber Pressure: 53.00 bar. Area Ratio: 18.9. Thrust to Weight Ratio: 74.4.
Related
- Country
- Russia
- Launch Vehicles
- Sputnik 8K71PS
- Propellants
- Lox/Kerosene
- Stages
- Sputnik 8K71PS-1
- Agency
- Glushko bureau
Photo Gallery
R-7 aft end
Credit: © Mark Wade
