Liberty-1

Engine · USA

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

Notional LOx/Kerosene rocket engine. Development ended 1988. Pressure-fed engine. Used on Liberty launch vehicle.

Thrust (sl): 208.800 kN (46,940 lbf). Thrust (sl): 21,296 kgf. Engine: 270 kg (590 lb). Area Ratio: 5. Thrust to Weight Ratio: 92.59.

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