CZ-2E(A)-0 (original) (raw)

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CZ-2E(A)-0

Part of CZ-2-0 stage series

N2O4/UDMH propellant rocket stage. .

Status: Design 2000. Thrust: 1,632.80 kN (367,068 lbf). Gross mass: 80,000 kg (176,000 lb). Unfuelled mass: 8,000 kg (17,600 lb). Specific impulse: 291 s. Specific impulse sea level: 261 s. Burn time: 125 s. Height: 27.00 m (88.00 ft). Diameter: 2.25 m (7.38 ft). Span: 2.26 m (7.41 ft).

No Engines: 2.

Country: China. Engines: YF-20B. Launch Vehicles: Chang Zheng 2E(A). Propellants: N2O4/UDMH.

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