RD-107-8D74PS
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-0. Out of Production. OKB Glushko. Used on 8K71PS Stage 0. Developed in 1956-1957. Flown 1957-1958. Propellants kerosene (RG-1) / LOx. Diameter is per chamber.
Chambers: 4. Thrust (sl): 793.200 kN (178,318 lbf). Thrust (sl): 80,884 kgf. Engine: 1,155 kg (2,546 lb). Chamber Pressure: 60.00 bar. Area Ratio: 18.9. Thrust to Weight Ratio: 85.71.
Related
- Country
- Russia
- Launch Vehicles
- Sputnik 8K71PS
- Propellants
- Lox/Kerosene
- Agency
- Glushko bureau
Photo Gallery
R-7 aft end
Credit: © Mark Wade
