CZ-2C/SD-2 (original) (raw)

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CZ-2C/SD-2

Part of CZ-2-2 stage series

N2O4/UDMH propellant rocket stage. Stretched version of CZ-2C second stage. Empty mass estimated.

AKA: L-35. Status: Development ended 1997. Thrust: 761.90 kN (171,282 lbf). Gross mass: 55,000 kg (121,000 lb). Unfuelled mass: 5,000 kg (11,000 lb). Specific impulse: 298 s. Specific impulse sea level: 270 s. Burn time: 190 s. Height: 10.00 m (32.00 ft). Diameter: 3.35 m (10.99 ft). Span: 3.35 m (10.99 ft).

Country: China. Engines: YF-22A/23A. Launch Vehicles: Chang Zheng 3B, Chang Zheng 2C-III/SD, Chang Zheng 3C. Propellants: N2O4/UDMH.

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