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CZ-3A-3
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Gross Mass: 21,000 kg (46,000 lb). Empty Mass: 2,800 kg (6,100 lb). Thrust (vac): 156.000 kN (35,070 lbf). Isp: 440 sec. Burn time: 470 sec. Propellants: Lox/LH2. Diameter: 3.00 m (9.80 ft). Span: 3.00 m (9.80 ft). Length: 12.38 m (40.60 ft). Country: China. No Engines: 2. Engine: YF-75. Status: Development ended 1997. Cost $ : 16.000 million. First Flight: 1994. Last Flight: 2006. No Launched: 17. Other designations: H-18.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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