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Used on stages: LCLV-2. Used on launch vehicles: LCLV. Propellants: N2O4/UDMH Thrust(vac): 998,639 kgf. Thrust(vac): 9,793.20 kN. Isp: 300 sec. Isp (sea level): 240 sec. Diameter: 4.6 m. Chambers: 1. Chamber Pressure: 17.01 bar. Area Ratio: 31.00. 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 .