This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Used on stages: Sergeant. Used on launch vehicles: Juno II, Jupiter C. Gross Mass: 42 kg. Empty Mass: 21 kg. Propellants: Solid Thrust(vac): 680 kgf. Thrust(vac): 6.66 kN. Isp: 235 sec. Isp (sea level): 214 sec. Burn time: 6 sec. Diameter: 0.3 m. Length: 1.0 m. Chambers: 1. Country: USA. Status: Out of Production. First Flight: 1956. Last Flight: 1961. Flown: 285. Comments: Used in Jupiter C, Juno 2.
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Last update 12 March 2001.
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© Mark Wade, 2001 .