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RD-107-8D74K
Part of RD-107
RD-107 Credit: © Mark Wade |
Glushko LOx/Kerosene rocket engine. Developed in 1957-1960. Used in strap-ons for Molniya 8K78, R-7A 8K74, Voskhod 11A57, Vostok 8A92, Vostok 8A92M. Fuel T-1 or RG-1 kerosene. First flight 1959.
AKA: 8D74K. Number: 1952 . Thrust: 996.00 kN (223,909 lbf). Unfuelled mass: 1,145 kg (2,524 lb). Specific impulse: 313 s. Specific impulse sea level: 256 s. Burn time: 119 s. Height: 2.86 m (9.38 ft). Diameter: 0.67 m (2.19 ft).
Diameter is per chamber.
Chambers: 4. Thrust (sl): 814.000 kN (182,994 lbf). Thrust (sl): 83,016 kgf. Engine: 1,145 kg (2,524 lb). Chamber Pressure: 59.70 bar. Area Ratio: 18.9. Thrust to Weight Ratio: 88.64.
Country:
Russia.
Launch Vehicles:
R-7A,
Molniya 8K78,
Voskhod 11A57,
Vostok 8A92,
Sputnik 11A59,
Vostok 8A92M.
Propellants:
Lox/Kerosene.
Stages:
Molniya 8K78-0,
R-7A 8K74-0,
Vostok 8A92-0,
Voskhod 11A57-0,
Vostok 8A92M-0.
Agency:
Glushko bureau.
Photo Gallery
| R-7 aft end Credit: © Mark Wade |
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