This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Used on stages: LCLV-1. Used on launch vehicles: LCLV. Propellants: N2O4/UDMH Thrust(vac): 5,748,000 kgf. Thrust(vac): 56,368.00 kN. Isp: 267 sec. Isp (sea level): 245 sec. Diameter: 6.1 m. Chambers: 1. Chamber Pressure: 20.41 bar. Area Ratio: 6.00. Thrust to Weight Ratio: 0.00. Country: USA. Status: Design concept 1960's. Comments: 1960's designs for 'big dumb booster'..
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Last update 12 March 2001.
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© Mark Wade, 2001 .