This page no longer updated from 31 October 2001.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

Gross Mass: 600,800 kg. Empty Mass: 60,000 kg. Thrust (vac): 650,675 kgf. Isp: 421 sec. Burn time: 345 sec. Propellants: Lox/LH2 Isp(sl): 200 sec. Diameter: 10.1 m. Span: 10.1 m. Length: 29.6 m. Country: USA. No Engines: 7. J-2 Status: Study NASA 1966. Comments: Basic Saturn II with 187 inch stretch of propellant tanks, 1.2 million pound propellant capacity, and 7 J-2 engines.
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Last update 12 March 2001.
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© Mark Wade, 2001 .