This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Gross Mass: 306,000 kg.
Empty Mass: 20,000 kg. Thrust (vac): 551,273 kgf. Isp: 330 sec. Burn time: 170 sec. Propellants: Lox/Kerosene Isp(sl): 293 sec. Diameter: 4.5 m. Span: 7.5 m. Length: 29.0 m. Country: China. No Engines: 4. Status: Study 1992. Comments: Engine chamber pressure 13 to 15 Mpa.
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Last update 12 March 2001.
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© Mark Wade, 2001 .