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RD-114
Part of RD-107 Family
Glushko LOx/UDMH rocket engine. Used in ICBM stage 1 (stage 2 was RD-115). Developed 1961-65.

Status: Developed 1961-65. Date: 1961-65. Thrust: 1,653.00 kN (371,609 lbf). Unfuelled mass: 990 kg (2,180 lb). Specific impulse: 341 s. Specific impulse sea level: 307 s. Burn time: 120 s. Height: 2.60 m (8.50 ft). Diameter: 1.46 m (4.80 ft).

Engine: 990 kg (2,180 lb). Chamber Pressure: 147.00 bar. Area Ratio: 26.4. Thrust to Weight Ratio: 170.26. Oxidizer to Fuel Ratio: 1.77.



Country: Russia. Propellants: Lox/UDMH. Agency: Glushko bureau. Bibliography: 320.

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