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CZ-2C/SD-2
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Gross Mass: 55,000 kg (121,000 lb). Empty Mass: 5,000 kg (11,000 lb). Thrust (vac): 761.900 kN (171,282 lbf). Isp: 298 sec. Burn time: 190 sec. Propellants: N2O4/UDMH. Isp(sl): 270 sec. Diameter: 3.35 m (10.99 ft). Span: 3.35 m (10.99 ft). Length: 10.00 m (32.00 ft). Country: China. No Engines: 1. Engine: YF-22A/23A. Status: Out of production. First Flight: 1996. Last Flight: 2006. No Launched: 14. Other designations: L-35. Stretched version of CZ-2C second stage. Empty mass estimated.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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