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Engine Model: RD-114. Manufacturer Name: RD-114. Designer: Glushko. Developed in: 1961-65. Application: Used in ICBM stage 1 (stage 2 was RD-115). Propellants: Lox/UDMH. Thrust(vac): 1,653.000 kN (371,609 lbf). Isp: 341 sec. Isp (sea level): 307 sec. Burn time: 120 sec. Mass Engine: 990 kg (2,180 lb). Diameter: 1.46 m (4.80 ft). Length: 2.60 m (8.50 ft). Chambers: 1. Chamber Pressure: 147.00 bar. Area Ratio: 26.40. Oxidizer to Fuel Ratio: 1.77. Thrust to Weight Ratio: 170.26. Country: Russia. Status: Developed 1961-65.
Bibliography:- Glushko, V P, Albom Konstruktsiy ZhRD, Vol. 1 1968, Vol. 3 & 4 1969 via Dietrich Haeseler.
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