This page no longer updated from 31 October 2001.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

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.
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Last update 12 March 2001.
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© Mark Wade, 2001 .