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RD-108-8D75PS
Part of RD-107
RD-107 Credit: © Mark Wade |
Glushko LOx/Kerosene rocket engine. Sputnik 8K71PS-1. Out of Production. Diameter is per chamber. First flight 1957.
AKA: 8D75PS. Status: Out of Production. Number: 32 . Thrust: 912.00 kN (205,025 lbf). Unfuelled mass: 1,250 kg (2,750 lb). Specific impulse: 308 s. Specific impulse sea level: 241 s. Burn time: 340 s. Height: 2.86 m (9.38 ft). Diameter: 0.67 m (2.19 ft).
Chambers: 4. Thrust (sl): 713.600 kN (160,424 lbf). Thrust (sl): 72,768 kgf. Engine: 1,250 kg (2,750 lb). Chamber Pressure: 53.00 bar. Area Ratio: 18.9. Thrust to Weight Ratio: 74.4.
Country:
Russia.
Launch Vehicles:
Sputnik 8K71PS.
Propellants:
Lox/Kerosene.
Stages:
Sputnik 8K71PS-1.
Agency:
Glushko bureau.
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