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CZ-1D-2
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Gross Mass: 14,850 kg (32,730 lb). Empty Mass: 2,650 kg (5,840 lb). Thrust (vac): 294.000 kN (66,093 lbf). Isp: 287 sec. Burn time: 120 sec. Propellants: N2O4/UDMH. Isp(sl): 260 sec. Diameter: 2.25 m (7.38 ft). Span: 2.25 m (7.38 ft). Length: 5.35 m (17.55 ft). Country: China. No Engines: 1. Engine: YF-3. Status: Out of production. Cost $ : 1.000 million. First Flight: 1995. Last Flight: 2002. No Launched: 3.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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