This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Used on stages: CZ-1C-3. Used on launch vehicles: CZ-1C. Propellants: N2O4/UDMH Thrust(vac): 11,000 kgf. Thrust(vac): 107.90 kN. Isp: 287 sec. Isp (sea level): 258 sec. Burn time: 164 sec. Diameter: 1.8 m. Chambers: 1. Country: China. Status: Developed to 1984.
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Last update 12 March 2001.
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© Mark Wade, 2001 .