This page no longer updated from 31 October 2001. Latest version can be found at MBB-ATC500

Designer: MBB. Used on stages: Beta. Used on launch vehicles: Beta. Propellants: Lox/LH2 Thrust(vac): 45,000 kgf. Thrust(vac): 441.30 kN. Isp: 460 sec. Isp (sea level): 409 sec. Burn time: 318 sec. Chambers: 1. Chamber Pressure: 250.00 bar. Country: Germany. Status: Study 1980.
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 .