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Gross Mass: 1,814,000 kg.
Empty Mass: 125,000 kg. Thrust (vac): 3,084,000 kgf. Isp: 304 sec. Burn time: 164 sec. Propellants: Lox/Kerosene Isp(sl): 265 sec. Diameter: 13.7 m. Span: 13.7 m. Length: 35.1 m. Country: USA. No Engines: 4. F-1 Status: Study, NASA, 1960. Comments: Masses estimated based on total vehicle thrust, performance, and stage volumes. .
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Last update 12 March 2001.
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© Mark Wade, 2001 .