This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Gross Mass: 272,000 kg.
Empty Mass: 28,000 kg. Thrust (vac): 200,000 kgf. Isp: 455 sec. Burn time: 550 sec. Propellants: Lox/LH2 Isp(sl): 352 sec. Diameter: 7.7 m. Span: 7.7 m. Length: 20.0 m. Country: Russia. No Engines: 1. RD-0120M Status: Develop.
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Last update 12 March 2001.
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© Mark Wade, 2001 .