This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Gross Mass: 91,687 kg.
Empty Mass: 3,995 kg. Thrust (vac): 125,647 kgf. Isp: 459 sec. Burn time: 300 sec. Propellants: Lox/LH2 Isp(sl): 359 sec. Diameter: 6.7 m. Span: 6.7 m. Length: 18.9 m. Country: USA. No Engines: 1. Plug-Nozzle SASSTO Status: Study. Other designations: Saturn Applications Single Stage to Orbit. Comments: Recoverable S-IVB with plug nozzle engine.
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Last update 12 March 2001.
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© Mark Wade, 2001 .