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RD-107-8D74-1959
Part of RD-107 Family
Glushko LOx/Kerosene rocket engine. Out of production. Diameter is per chamber. Used on Vostok 8K72K launch vehicle. First flight 1960.

AKA: 8D74-1959. Status: Out of production. Number: 52 . Thrust: 996.00 kN (223,909 lbf). Unfuelled mass: 1,155 kg (2,546 lb). Specific impulse: 313 s. Specific impulse sea level: 256 s. Burn time: 120 s. Height: 2.86 m (9.38 ft). Diameter: 0.67 m (2.19 ft).

Chambers: 4. Engine: 1,155 kg (2,546 lb). Chamber Pressure: 58.60 bar. Area Ratio: 18.9. Thrust to Weight Ratio: 87.87. Oxidizer to Fuel Ratio: 2.47.



Country: Russia. Launch Vehicles: Vostok 8K72K. Propellants: Lox/Kerosene. Stages: Vostok 8K72K-0. Agency: Glushko bureau.

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