This page no longer updated from 31 October 2001. Latest version can be found at Co-axial turboramjet

Used on stages: Sanger II-1. Used on launch vehicles: Sanger II. Propellants: Air/LH2 Thrust(vac): 25,492 kgf. Thrust(vac): 250.00 kN. Isp: 1,200 sec. Isp (sea level): 3,600 sec. Burn time: 6,565 sec. Chambers: 1. Country: Germany. Status: Study -1985.
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Last update 12 March 2001.
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© Mark Wade, 2001 .