This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com

astronautix.com UR-700M-2


Gross Mass: 5,250,000 kg. Empty Mass: 500,000 kg. Thrust (vac): 10,402,500 kgf. Isp: 337 sec. Burn time: 200 sec. Propellants: Lox/Kerosene Isp(sl): 311 sec. Diameter: 12.5 m. Span: 30.5 m. Length: 30.0 m. Country: Russia. No Engines: 16. RLA-600 Status: Design 1972. Comments: Total mass, length, estimated based on empty mass, total vehicle mass. Engine specific impulse estimated based on follow-on RD-170 engines.
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Last update 12 March 2001.
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© Mark Wade, 2001 .