This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
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'..
Back to Index
Last update 12 March 2001.
Definitions of Technical Terms.
Contact Mark Wade with any corrections or comments.
Conditions for use of drawings, pictures, or other materials from this site..
© Mark Wade, 2001 .