This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Used on stages: Tu-2000, X-30. Used on launch vehicles: Tu-2000, X-30. Propellants: Air/Slush LH2 Thrust(vac): 140,000 kgf. Thrust(vac): 1,372.90 kN. Isp: 1,550 sec. Burn time: 886 sec. Diameter: 16.0 m. Chambers: 1. Country: USA. Status: Developed 1984-1989. Comments: Thrust is maximum sea level thrust; specific impulse is average during ascent.
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 .