This page no longer updated from 31 October 2001. Latest version can be found at Saturn II-INT-17

Gross Mass: 495,000 kg. Empty Mass: 48,000 kg. Thrust (vac): 990,500 kgf. Isp: 450 sec. Burn time: 200 sec. Propellants: Lox/LH2 Isp(sl): 275 sec. Diameter: 10.1 m. Span: 10.1 m. Length: 24.8 m. Country: USA. No Engines: 7. HG-3-SL Status: Study 1966. Comments: Saturn II modifed with reduced expansion ratio HG-3 high pressure engines for use a first stage (sea level launch).
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Last update 12 March 2001.
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© Mark Wade, 2001 .