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Sanger-Bredt Sled
Saenger LOx/Alcohol rocket engine. Study 1943. Used on Sanger launch vehicle.

Status: Study 1943. Thrust: 1,144.10 kN (257,204 lbf). Specific impulse: 245 s. Specific impulse sea level: 210 s. Burn time: 10 s.

Thrust (sl): 980.600 kN (220,448 lbf). Thrust (sl): 99,999 kgf.



People: Saenger. Country: Germany. Launch Vehicles: Saenger Antipodal Bomber. Propellants: Lox/Alcohol. Stages: Sanger Sled.

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