| CZ-NGLV-KO |
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Model: CZ-NGLV-KO. Gross Mass: 60,000 kg (132,000 lb). Empty Mass: 7,000 kg (15,400 lb). Thrust (vac): 588.000 kN (132,187 lbf). Isp: 340 sec. Burn time: 300 sec. Propellants: Lox/Kerosene. Diameter: 3.35 m (10.99 ft). Span: 3.35 m (10.99 ft). Length: 13.00 m (42.00 ft). Country: China. No Engines: 4. Status: In development. First Flight: 2000. Last Flight: 2000. No Launched: 1. Upper stage for the 3.35 m diameter core vehicle. Only information available are the types of propellants, total thrust, and number of engines. Therefore all values shown here except thrust are estimated. This launcher has a low priority since its payload capability overlaps existing Chinese launch vehicles, and it would not be developed until after 2010. Used on Launch Vehicles: Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted. |