This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Gross Mass: 11,600,000 kg.
Empty Mass: 1,300,000 kg. Thrust (vac): 36,400,000 kgf. Isp: 290 sec. Burn time: 81 sec. Propellants: Lox/Kerosene Isp(sl): 200 sec. Diameter: 21.5 m. Span: 30.0 m. Length: 68.0 m. Country: USA. No Engines: 1. Sea Dragon-1 Status: Design. Comments: Sea level thrust shown. Thrust, chamber pressure varies during ascent. Vacuum thrust at cut-off 40 million kgf. Total mass, specific impulse estimated from booster performance figures.
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Last update 12 March 2001.
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© Mark Wade, 2001 .