This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Used on stages: Sanger-Bredt. Used on launch vehicles: Sanger. Propellants: Lox/Kerosene Thrust(vac): 145,700 kgf. Thrust(vac): 1,428.80 kN. Isp: 306 sec. Isp (sea level): 210 sec. Burn time: 168 sec. Chambers: 1. Country: Germany. Status: Study 1942. Comments: Used in Sanger-Bredt.
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Last update 12 March 2001.
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© Mark Wade, 2001 .