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CZ-4A-2
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Gross Mass: 39,550 kg (87,190 lb). Empty Mass: 4,000 kg (8,800 lb). Thrust (vac): 831.005 kN (186,817 lbf). Isp: 295 sec. Burn time: 135 sec. Propellants: N2O4/UDMH. Isp(sl): 260 sec. Diameter: 3.35 m (10.99 ft). Span: 3.35 m (10.99 ft). Length: 10.41 m (34.15 ft). Country: China. No Engines: 1. Engine: YF-25/23. Status: In production. Cost $ : 3.000 million. First Flight: 1988. Last Flight: 2005. No Launched: 9. Other designations: L-35.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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