This page no longer updated from 31 October 2001. Latest version can be found at RD-211

Manufacturer Name: RD-211. Designer: Glushko. Developed in: 1952-55. Application: long-distance missile. Propellants: Nitric acid/Kerosene Thrust(vac): 65,500 kgf. Thrust(vac): 642.30 kN. Isp: 262 sec. Isp (sea level): 224 sec. Burn time: 122 sec. Mass Engine: 635 kg. Diameter: 1.6 m. Length: 2.7 m. Chamber Pressure: 39.20 bar. Area Ratio: 9.52. Oxidizer to Fuel Ratio: 4.05. Country: Russia. Status: Developed 1952-55. References: 320 .
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Last update 12 March 2001.
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© Mark Wade, 2001 .