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CZ-NGLV-522/HO
Part of CZ-NGLV
CZ-NGLV-522/HO
CZ-NGLV-522/HO
Credit: © Mark Wade
Chinese orbital launch vehicle. The 522/HO was the 'all up' baseline configuration for the Long March New Generation Launch Vehicle series. It would use the 5.0 m core stage, topped by the 5.0 m upper stage, together with 2 x 2.25 m plus 2 x 3.35 m strap-on stages. It was announced in 2003 that it would be first to fly, with a launch before the Beijing Olympics in 2008. It would be used for launch of large communications satellites. Payload is estimated as 10-12 metric tons to geosynchronous transfer orbit. Version dropped together with the 2.25 m booster module.

AKA: Chang Zheng Next Generation Launch Vehicle Type A;CZ-5-5.0;CZ-NGLV-A;Long March Next Generation Launch Vehicle Type A. Status: In development. Payload: 11,000 kg (24,000 lb). Thrust: 8,240.00 kN (1,852,420 lbf). Gross mass: 630,000 kg (1,380,000 lb). Height: 58.00 m (190.00 ft). Diameter: 5.00 m (16.40 ft). Span: 13.00 m (42.00 ft).

Payload: 11,000 kg (24,000 lb) to a GTO.

Stage Data - CZ-NGLV-522/HO



Family: orbital launch vehicle. Country: China. Engines: YF-120t, YF-50t, YF-75. Stages: CZ-NGLV-300, CZ-NGLV-500, CZ-NGLV-200 stage, CZ-NGLV-HO. Agency: CALT.

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