This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Gross Mass: 123,800 kg.
Empty Mass: 28,600 kg. Thrust (vac): 233,000 kgf. Isp: 439 sec. Burn time: 886 sec. Propellants: Lox/LH2 Isp(sl): 339 sec. Diameter: 20.7 m. Span: 20.7 m. Length: 20.4 m. Country: USA. No Engines: 2. XRS-2200 Status: Development.
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 .