This page no longer updated from 31 October 2001.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

Gross Mass: 521,447 kg. Empty Mass: 49,877 kg. Thrust (vac): 526,764 kgf. Isp: 425 sec. Burn time: 361 sec. Propellants: Lox/LH2 Isp(sl): 306 sec. Diameter: 10.1 m. Span: 10.1 m. Length: 25.9 m. Country: USA. No Engines: 5. J-2 Status: Study NASA 1966. Comments: Basic Saturn II with 41 inch stretch of hydrogen tank.
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Last update 12 March 2001.
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© Mark Wade, 2001 .