This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Propellants: Lox/LH2 Thrust(vac): 254,020 kgf. Thrust(vac): 2,491.00 kN. Isp: 447 sec. Isp (sea level): 200 sec. Burn time: 204 sec. Chambers: 1. Country: USA. Status: Design concept 1990's.
Back to Index
Last update 12 March 2001.
Definitions of Technical Terms.
Contact Mark Wade with any corrections or comments.
Conditions for use of drawings, pictures, or other materials from this site..
© Mark Wade, 2001 .