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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): 168,559 kgf. Thrust(vac): 1,653.00 kN. Isp: 341 sec. Isp (sea level): 307 sec. Burn time: 120 sec. Mass Engine: 990 kg. Diameter: 1.5 m. Length: 2.6 m. Chambers: 1. Chamber Pressure: 147.00 bar. Area Ratio: 26.40. Oxidizer to Fuel Ratio: 1.77. Country: Russia. Status: Developed 1961-65. References: 320 .
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Last update 12 March 2001.
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© Mark Wade, 2001 .