This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Gross Mass: 474,199 kg.
Empty Mass: 100,153 kg. Thrust (vac): 721,903 kgf. Isp: 459 sec. Burn time: 234 sec. Propellants: Lox/LH2 Isp(sl): 359 sec. Diameter: 8.1 m. Span: 29.6 m. Length: 47.9 m. Country: USA. No Engines: 3. SSME Study Status: Study. Comments: Delta wing configuration with drop tanks - Cross Range 1,774 km.
Back to Index
Last update 12 March 2001.
Contact Mark Wade with any corrections or comments.
Conditions for use of drawings, pictures, or other materials from this site..
© Mark Wade, 2001 .