This page no longer updated from 31 October 2001. Latest version can be found at Saturn MS-IC-1

Advanced Engines
Advanced Engines
Advanced Engines planned for uprated Saturn and Nova boosters

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Gross Mass: 2,694,703 kg. Empty Mass: 169,719 kg. Thrust (vac): 4,685,469 kgf. Isp: 310 sec. Burn time: 158 sec. Propellants: Lox/Kerosene Isp(sl): 270 sec. Diameter: 10.1 m. Span: 19.0 m. Length: 48.1 m. Country: USA. No Engines: 5. F-1A Status: Study NASA 1966. Comments: Basic Saturn IC stretched 240 inches with F-1A engines uprated 20% in thrust and 6 second improvement in specific impulse.
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Last update 12 March 2001.
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© Mark Wade, 2001 .