This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Gross Mass: 342,948 kg.
Empty Mass: 129,329 kg. Thrust (vac): 481,269 kgf. Isp: 459 sec. Burn time: 201 sec. Propellants: Lox/LH2 Isp(sl): 359 sec. Diameter: 7.5 m. Span: 29.7 m. Length: 48.3 m. Country: USA. No Engines: 2. SSME Study Status: Study. Comments: Delta winged configuration.
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 .