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Engine Model: Sanger-Bredt. Propellants: Lox/Kerosene. Thrust(vac): 1,428.800 kN (321,207 lbf). Thrust(sl): 980.600 kN (220,448 lbf). Isp: 306 sec. Isp (sea level): 210 sec. Burn time: 168 sec. Chambers: 1. Country: Germany. Status: Study 1943. Used in Sanger-Bredt.
Sanger-Bredt used on Rocket Stages
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