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Gross Mass: 506,000 kg.
Empty Mass: 50,000 kg. Thrust (vac): 1,405,000 kgf. Isp: 347 sec. Burn time: 106 sec. Propellants: Lox/Kerosene Diameter: 6.8 m. Span: 9.8 m. Length: 20.0 m. Country: Russia. No Engines: 8. NK-15V Status: Design 1962. Comments: Includes 3500 kg Stage 2-Stage 3 interstage. Compared to total fuelled mass excludes 1,000 kg in propellants lost to boil-off prior to stage ignition. Values as in draft project as defended on 2-16 July 1962.
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Last update 12 March 2001.
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© Mark Wade, 2001 .