Liberty-2

Engine · USA

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

Notional N2O4/MMH rocket engine. Development ended 1988. Pressure-fed engine. Used on Liberty launch vehicle.

Thrust (sl): 11.900 kN (2,675 lbf). Thrust (sl): 1,209 kgf. Engine: 41 kg (90 lb). Area Ratio: 98. Thrust to Weight Ratio: 44.34.

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