| Chang Cheng 1 |
home
topic index |
|
Model: Chang Cheng 1. Gross Mass: 57,000 kg (125,000 lb). Empty Mass: 30,000 kg (66,000 lb). Thrust (vac): 490.000 kN (110,150 lbf). Isp: 230 sec. Burn time: 430 sec. Propellants: Lox/LH2. Diameter: 4.50 m (14.70 ft). Span: 17.00 m (55.00 ft). Length: 24.00 m (78.00 ft). Country: China. No Engines: 1. Status: Design 1988. All characteristics except dimensions estimated, on assumption that stage used same propulsion systems as Shanghai upper stage. 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. |