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RD-112
Part of RD-107 Family
Glushko LOx/UDMH rocket engine. ICBM stage 1 (stage 2 was RD-113). Developed 1960.

Status: Developed 1960. Date: 1960. Thrust: 1,089.00 kN (244,816 lbf). Unfuelled mass: 790 kg (1,740 lb). Specific impulse: 344 s. Specific impulse sea level: 304 s. Height: 2.60 m (8.50 ft). Diameter: 1.29 m (4.23 ft).

Engine: 790 kg (1,740 lb). Chamber Pressure: 147.00 bar. Area Ratio: 31.8. Thrust to Weight Ratio: 140.56. Oxidizer to Fuel Ratio: 1.704.



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

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