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CZ-4A-3
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Gross Mass: 15,150 kg (33,400 lb). Empty Mass: 1,000 kg (2,200 lb). Thrust (vac): 100.810 kN (22,663 lbf). Isp: 303 sec. Burn time: 400 sec. Propellants: N2O4/UDMH. Isp(sl): 260 sec. Diameter: 2.90 m (9.50 ft). Span: 2.90 m (9.50 ft). Length: 1.92 m (6.29 ft). Country: China. No Engines: 2. Engine: YF-40. Status: Out of production. Cost $ : 1.500 million. First Flight: 1988. Last Flight: 1990. No Launched: 2. Other designations: L-14.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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