MBB-ATC500

Engine · Germany

Original archive entry. The text, images and links below are kept as they were written.

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

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

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