CZ-1C-3

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Model: CZ-1C-3. Gross Mass: 6,400 kg (14,100 lb). Empty Mass: 1,000 kg (2,200 lb). Thrust (vac): 107.000 kN (24,054 lbf). Isp: 287 sec. Burn time: 164 sec. Propellants: N2O4/UDMH. Isp(sl): 258 sec. Diameter: 1.80 m (5.90 ft). Span: 1.80 m (5.90 ft). Length: 4.50 m (14.70 ft). Country: China. No Engines: 1. Motor: CZ-1C-3. Status: Development ended 1988. Cost $ : 0.600 million. First Flight: 1984. Used on Launch Vehicles: CZ-1. Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted.