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

Status: Developed 1960. Date: 1960. Thrust: 1,138.00 kN (255,832 lbf). Unfuelled mass: 1,100 kg (2,400 lb). Specific impulse: 360 s. Height: 4.20 m (13.70 ft). Diameter: 2.48 m (8.13 ft).

Engine: 1,100 kg (2,400 lb). Chamber Pressure: 147.00 bar. Area Ratio: 119.8. Thrust to Weight Ratio: 105.49. Oxidizer to Fuel Ratio: 1.704.



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

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