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Gross Mass: 2,217,285 kg.
Empty Mass: 131,495 kg. Thrust (vac): 3,901,230 kgf. Isp: 304 sec. Burn time: 160 sec. Propellants: Lox/Kerosene Isp(sl): 265 sec. Diameter: 10.1 m. Span: 19.0 m. Length: 42.9 m. Country: USA. No Engines: 5. F-1 Status: Study 1961. Used as: Saturn C-5A-1. Comments: Final first stage design of Saturn C-5 (November 1961) before selection as Apollo launch vehicle and development in Saturn V.
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Last update 12 March 2001.
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© Mark Wade, 2001 .