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ATCRE
Notional LOx/LH2 rocket engine. Study 1985. Used on Sanger II launch vehicle.

Status: Study 1985. Thrust: 1,280.00 kN (287,750 lbf). Specific impulse: 490 s. Specific impulse sea level: 409 s. Burn time: 298 s.

Thrust (sl): 1,068.400 kN (240,186 lbf). Thrust (sl): 108,948 kgf. Chamber Pressure: 282.00 bar.



Country: Germany. Launch Vehicles: Saenger II. Propellants: Lox/LH2. Stages: Sanger II-2.

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