This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
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.
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Last update 12 March 2001.
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© Mark Wade, 2001 .