This page no longer updated from 31 October 2001. Latest version can be found at Project 921-2

Gross Mass: 57,000 kg. Empty Mass: 7,000 kg. Thrust (vac): 50,000 kgf. Isp: 440 sec. Burn time: 430 sec. Propellants: Lox/LH2 Diameter: 4.5 m. Span: 4.5 m. Length: 10.0 m. Country: China. No Engines: 1. Status: Study 1992. Comments: Additionally 4 vernier Lox/LH2 engines with a total thrust of 4600 kgf and a storable engine package for stage propellant ullage and restart.
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Last update 12 March 2001.
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© Mark Wade, 2001 .