RD-108-8D77
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 8A91-1. Out of Production. Diameter is per chamber. First flight 1958.
Chambers: 4. Thrust (sl): 628.000 kN (141,180 lbf). Thrust (sl): 64,040 kgf. Engine: 1,250 kg (2,750 lb). Chamber Pressure: 39.20 bar. Area Ratio: 18.9. Thrust to Weight Ratio: 65.6.
Related
- Country
- Russia
- Launch Vehicles
- Sputnik 8A91
- Propellants
- Lox/Kerosene
- Stages
- Sputnik 8A91-1
- Agency
- Glushko bureau
Photo Gallery
R-7 aft end
Credit: © Mark Wade
