This page no longer updated from 31 October 2001. Latest version can be found at OOST ISI

Gross Mass: 5,125,000 kg. Empty Mass: 292,000 kg. Thrust (vac): 8,707,000 kgf. Isp: 455 sec. Burn time: 248 sec. Propellants: Lox/LH2 Isp(sl): 365 sec. Diameter: 21.3 m. Span: 21.3 m. Length: 57.9 m. Country: USA. No Engines: 15. Chamber/single nozzle Status: Study 1963. Comments: .
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Last update 12 March 2001.
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© Mark Wade, 2001 .