This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Designer: Beijing Wan Yuan Industry Corp. Used on stages: CZ-1-3. Used on launch vehicles: CZ-1. Gross Mass: 2,000 kg. Empty Mass: 200 kg. Propellants: Solid Thrust(vac): 2,957 kgf. Thrust(vac): 29.00 kN. Isp: 230 sec. Isp (sea level): 200 sec. Burn time: 140 sec. Diameter: 0.8 m. Length: 2.0 m. Chambers: 1. Country: China. Status: Out of Production. First Flight: 1970. Last Flight: 1971. Flown: 3.
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Last update 12 March 2001.
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© Mark Wade, 2001 .