This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Used on stages: AMROC. Used on launch vehicles: Industrial Launch Vehicle. Propellants: Lox/Solid Thrust(vac): 94,970 kgf. Thrust(vac): 931.30 kN. Isp: 284 sec. Isp (sea level): 283 sec. Burn time: 75 sec. Diameter: 1.8 m. Chambers: 1. Country: USA. Status: Developed -1989.
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Last update 12 March 2001.
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© Mark Wade, 2001 .