This page no longer updated from 31 October 2001. Latest version can be found at NOTS-1

Used on stages: Caleb-1. Used on launch vehicles: Caleb. Gross Mass: 1,033 kg. Empty Mass: 194 kg. Propellants: Solid Thrust(vac): 5,441 kgf. Thrust(vac): 53.40 kN. Isp: 204 sec. Isp (sea level): 204 sec. Burn time: 34 sec. Diameter: 0.6 m. Chambers: 1. Country: USA. Status: Out of Production. First Flight: 1960. Last Flight: 1962. Flown: 5.
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Last update 12 March 2001.
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© Mark Wade, 2001 .