This page no longer updated from 31 October 2001. Latest version can be found at Buran M-41

Gross Mass: 18,000 kg. Empty Mass: 3,000 kg. Thrust (vac): 77,000 kgf. Isp: 254 sec. Burn time: 50 sec. Propellants: Nitric acid/Kerosene Isp(sl): 231 sec. Diameter: 1.2 m. Span: 3.0 m. Length: 19.1 m. Country: Russia. No Engines: 1. RD-213 Status: Cancelled November 1957. Comments: Booster for Buran missile. Four used to boost ramjet second stage to ignition conditions. Masses estimated based on missile known total mass. Specific impulse estimated.
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Last update 12 March 2001.
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© Mark Wade, 2001 .