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CZ-2E-0
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Gross Mass: 41,000 kg (90,000 lb). Empty Mass: 3,200 kg (7,000 lb). Thrust (vac): 816.285 kN (183,508 lbf). Isp: 291 sec. Burn time: 128 sec. Propellants: N2O4/UDMH. Isp(sl): 261 sec. Diameter: 2.25 m (7.38 ft). Span: 2.26 m (7.41 ft). Length: 15.33 m (50.29 ft). Country: China. No Engines: 1. Engine: YF-20B. Status: In production. Cost $ : 2.750 million. First Flight: 1990. Last Flight: 2006. No Launched: 80. Other designations: LB-40.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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