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MBB-ATC500
MBB LOx/LH2 rocket engine. Study 1969. Used on Beta launch vehicle.

Status: Study 1969. Thrust: 441.30 kN (99,208 lbf). Specific impulse: 460 s. Specific impulse sea level: 409 s. Burn time: 318 s.

Thrust (sl): 392.400 kN (88,215 lbf). Thrust (sl): 40,011 kgf. Chamber Pressure: 250.00 bar.



Country: Germany. Engines: MBB-ATC500. Launch Vehicles: Beta. Propellants: Lox/LH2. Agency: MBB.

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