This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Gross Mass: 15,000 kg.
Empty Mass: 2,000 kg. Thrust (vac): 15,000 kgf. Isp: 425 sec. Burn time: 363 sec. Propellants: Lox/LH2 Isp(sl): 306 sec. Diameter: 3.0 m. Span: 3.0 m. Length: 10.0 m. Country: USA. No Engines: 1. Truax LH2 Status: Devel.
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Last update 12 March 2001.
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© Mark Wade, 2001 .