This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Gross Mass: 16,327 kg.
Empty Mass: 2,600 kg. Thrust (vac): 14,970 kgf. Isp: 444 sec. Burn time: 420 sec. Propellants: Lox/LH2 Isp(sl): 0 sec. Diameter: 4.3 m. Span: 4.3 m. Length: 6.0 m. Country: USA. No Engines: 2. RL-10A-3A Status: Devel.
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 .