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RD-107-8D74-1958
Part of RD-107 Family
RD-107
RD-107
Credit: © Mark Wade
Glushko LOx/Kerosene rocket engine. Luna 8K72-0. Out of production. Diameter is per chamber. First flight 1958.

AKA: 8D74-1958. Status: Out of production. Number: 36 . Thrust: 996.00 kN (223,909 lbf). Unfuelled mass: 1,155 kg (2,546 lb). Specific impulse: 312 s. Specific impulse sea level: 254 s. Burn time: 120 s. Height: 2.86 m (9.38 ft). Diameter: 0.67 m (2.19 ft).

Chambers: 4. Thrust (sl): 806.400 kN (181,286 lbf). Thrust (sl): 82,224 kgf. Engine: 1,155 kg (2,546 lb). Chamber Pressure: 58.40 bar. Area Ratio: 18.9. Thrust to Weight Ratio: 87.44. Oxidizer to Fuel Ratio: 2.47.



Country: Russia. Launch Vehicles: Vostok-L 8K72. Propellants: Lox/Kerosene. Stages: Luna 8K72-0. Agency: Glushko bureau.
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