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Gross Mass: 193,000 kg.
Empty Mass: 16,000 kg. Thrust (vac): 160,000 kgf. Isp: 347 sec. Burn time: 368 sec. Propellants: Lox/Kerosene Diameter: 4.8 m. Span: 6.8 m. Length: 12.0 m. Country: Russia. No Engines: 4. NK-19 Status: Design 1962. Comments: 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 .