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CZ-NGLV-540/HO
Part of CZ-NGLV
CZ-NGLV-540/HO
CZ-NGLV-540/HO
Credit: © Mark Wade
Chinese orbital launch vehicle. The 540/HO configuration for the Long March New Generation Launch Vehicle series would use the 5.0 m core stage, topped by the 5.0 m upper stage, together with 4 x 2.25 m strap-on stages. First flight of this version was expected after 2010. Payload was given as 6 metric tons to geosynchronous transfer orbit. This version was no longer mentioned when by 2016.

AKA: Chang Zheng Next Generation Launch Vehicle Type C;CZ-5-5.0;CZ-NGLV-C;Long March Next Generation Launch Vehicle Type C. Status: In development. Payload: 6,000 kg (13,200 lb). Thrust: 5,840.00 kN (1,312,880 lbf). Gross mass: 490,000 kg (1,080,000 lb). Height: 53.00 m (173.00 ft). Diameter: 5.00 m (16.40 ft). Span: 11.00 m (36.00 ft).

Payload: 6,000 kg (13,200 lb) to a GTO.

Stage Data - CZ-NGLV-540/HO



Family: orbital launch vehicle. Country: China. Engines: YF-100, YF-77, YF-75D. Stages: CZ-NGLV-500, CZ-NGLV-200 stage, CZ-NGLV-HO. Agency: CALT.

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