Encyclopedia Astronautica
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CZ-2C-1
Part of CZ-2-1 stage series Family
N2O4/UDMH propellant rocket stage. .

AKA: L-140. Status: Active. Thrust: 3,295.00 kN (740,745 lbf). Gross mass: 153,000 kg (337,000 lb). Unfuelled mass: 10,000 kg (22,000 lb). Specific impulse: 291 s. Specific impulse sea level: 261 s. Burn time: 122 s. Height: 20.52 m (67.32 ft). Diameter: 3.35 m (10.99 ft). Span: 6.00 m (19.60 ft).

Cost $ : 4.000 million. No Engines: 4.

Country: China. Engines: YF-20A. Launch Vehicles: Chang Zheng 2C, Chang Zheng 2C-III/SD. Propellants: N2O4/UDMH.



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