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CZ-1D-2
Part of CZ-1-2 Family
N2O4/UDMH propellant rocket stage. .

Status: Out of production. Thrust: 294.00 kN (66,093 lbf). Gross mass: 14,850 kg (32,730 lb). Unfuelled mass: 2,650 kg (5,840 lb). Specific impulse: 287 s. Specific impulse sea level: 260 s. Burn time: 120 s. Height: 5.35 m (17.55 ft). Diameter: 2.25 m (7.38 ft). Span: 2.25 m (7.38 ft).

Cost $ : 1.000 million.



Country: China. Engines: YF-3. Launch Vehicles: Chang Zheng 1D. Propellants: N2O4/UDMH.

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