RD-107-8D76
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 8A91-0. Out of Production. OKB Glushko. Used on 8A91 Stage 0. Developed in 1956-1957. Propellants kerosene (RG-1) / LOx. Diameter is per chamber. First flight 1958.
Chambers: 4. Thrust (sl): 789.200 kN (177,419 lbf). Thrust (sl): 80,476 kgf. Engine: 1,155 kg (2,546 lb). Chamber Pressure: 56.90 bar. Area Ratio: 18.9. Thrust to Weight Ratio: 85.71.
Related
- Country
- Russia
- Launch Vehicles
- Sputnik 8A91
- Propellants
- Lox/Kerosene
- Agency
- Glushko bureau
Photo Gallery
R-7 aft end
Credit: © Mark Wade
