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RD-108-8D75K
Part of RD-107
R-7 aft end
Credit: © Mark Wade
Glushko LOx/Kerosene rocket engine. Molniya 8K78-1, R-7A 8K74-1, Voskhod 11A57-1, Vostok 8A92-1, Vostok 8A92M-1. Diameter is per chamber. First flight 1959.
AKA: 8D75K. Number: 488 . Thrust: 941.00 kN (211,545 lbf). Unfuelled mass: 1,252 kg (2,760 lb). Specific impulse: 315 s. Specific impulse sea level: 248 s. Burn time: 340 s. Height: 2.86 m (9.38 ft). Diameter: 0.67 m (2.19 ft).
Chambers: 4. Thrust (sl): 740.400 kN (166,449 lbf). Thrust (sl): 75,504 kgf. Engine: 1,252 kg (2,760 lb). Chamber Pressure: 51.00 bar. Area Ratio: 18.9. Thrust to Weight Ratio: 76.59.
Country:
Russia.
Launch Vehicles:
R-7A,
Molniya 8K78,
Voskhod 11A57,
Vostok 8A92,
Sputnik 11A59,
Vostok 8A92M.
Propellants:
Lox/Kerosene.
Stages:
Molniya 8K78-1,
R-7A 8K74-1,
Vostok 8A92-1,
Voskhod 11A57-1,
Vostok 8A92M-1.
Agency:
Glushko bureau.
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| RD-107 Credit: © Mark Wade |
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