This page no longer updated from 31 October 2001. Latest version can be found at Shuttle SERV-1

Gross Mass: 2,040,816 kg. Empty Mass: 226,757 kg. Thrust (vac): 3,261,105 kgf. Isp: 455 sec. Burn time: 249 sec. Propellants: Lox/LH2 Isp(sl): 367 sec. Diameter: 18.3 m. Span: 27.4 m. Length: 20.3 m. Country: USA. No Engines: 1. Plug-Nozzle SERV Status: Study. Comments: Single stage to orbit, ballistic reentry.
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Last update 12 March 2001.
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© Mark Wade, 2001 .