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Engine Model: Liberty-2. Propellants: N2O4/MMH. Thrust(vac): 17.800 kN (4,002 lbf). Thrust(sl): 11.900 kN (2,675 lbf). Isp: 300 sec. Isp (sea level): 200 sec. Burn time: 326 sec. Mass Engine: 41 kg (90 lb). Diameter: 1.43 m (4.69 ft). Chambers: 1. Area Ratio: 98.00. Thrust to Weight Ratio: 44.34. Country: USA. Status: Development ended 1988. Pressure-fed engine.
Liberty-2 used on Rocket Stages
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© Mark Wade, 1997 - 2008 except where otherwise noted.
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