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CZ-3-2
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Gross Mass: 39,000 kg (85,000 lb). Empty Mass: 4,000 kg (8,800 lb). Thrust (vac): 761.900 kN (171,282 lbf). Isp: 295 sec. Burn time: 130 sec. Propellants: N2O4/UDMH. Isp(sl): 270 sec. Diameter: 3.35 m (10.99 ft). Span: 3.35 m (10.99 ft). Length: 9.71 m (31.85 ft). Country: China. No Engines: 1. Engine: YF-22A/23A. Status: Out of production. Cost $ : 2.000 million. First Flight: 1984. Last Flight: 2000. No Launched: 13. Other designations: L-35.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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