Chang Cheng stage 1

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Chang Cheng stage 1

Part of Chang Cheng 1

LOx/LH2 propellant rocket stage. All characteristics except dimensions estimated, on assumption that stage used same propulsion systems as Shanghai upper stage.

AKA: Chang Cheng 1. Status: Design 1988. Thrust: 490.00 kN (110,150 lbf). Gross mass: 57,000 kg (125,000 lb). Unfuelled mass: 30,000 kg (66,000 lb). Specific impulse: 230 s. Burn time: 430 s. Height: 24.00 m (78.00 ft). Diameter: 4.50 m (14.70 ft). Span: 17.00 m (55.00 ft).

Family: Chinese Manned Spacecraft, Spaceplane. Country: China. Launch Vehicles: Chang Cheng 1. Propellants: Lox/LH2. Agency: SAST.

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