CZ H-18 stage (original) (raw)

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CZ H-18 stage

Part of CZ H-18

LOx/LH2 propellant rocket stage. .

AKA: CZ H-18;H-18. Status: Development ended 1997. Thrust: 156.00 kN (35,070 lbf). Gross mass: 21,000 kg (46,000 lb). Unfuelled mass: 2,800 kg (6,100 lb). Specific impulse: 440 s. Burn time: 470 s. Height: 12.38 m (40.60 ft). Diameter: 3.00 m (9.80 ft). Span: 3.00 m (9.80 ft).

Cost $ : 16.000 million. No Engines: 2.

Country: China. Engines: YF-75. Launch Vehicles: Chang Zheng 3A, Chang Zheng 3B, Chang Zheng 3C. Propellants: Lox/LH2.

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