This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Used on stages: Sanger II-2. Used on launch vehicles: Sanger II. Propellants: Lox/LH2 Thrust(vac): 130,524 kgf. Thrust(vac): 1,280.00 kN. Isp: 490 sec. Isp (sea level): 409 sec. Burn time: 298 sec. Chambers: 1. Chamber Pressure: 282.00 bar. Country: Germany. Status: Study -1985.
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 .