This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Used on stages: Nova MM 14A-1. Used on launch vehicles: Nova MM 14A. Propellants: Solid Thrust(vac): 6,485,000 kgf. Thrust(vac): 63,595.00 kN. Isp: 263 sec. Isp (sea level): 234 sec. Burn time: 106 sec. Diameter: 7.6 m. Length: 58.1 m. Chambers: 1. Country: USA. Status: Study 1963. Comments: Operational date would have been April 1973.
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Last update 12 March 2001.
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© Mark Wade, 2001 .