CZ-NGLV-HO

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CZ-NGLV-HO

Part of CZ H-18

LOx/LH2 propellant rocket stage. The upper stage for the Chinese Next Generation Launch Vehicle is a modification of the CZ-3B upper stage. The stage uses a version of the LOx/LH2 YF-75 engine, simplified for improved reliability. The stage is of hammerhead form, with the upper LH2 tank with a diameter of 5 m, and the lower liquid oxygen tank with a diameter of 3.35 m. The total propellant is 22,900 kg with a burn time of over 600 seconds. Empty mass has not yet been released and is estimated.

Status: In development. Thrust: 156.00 kN (35,070 lbf). Gross mass: 26,000 kg (57,000 lb). Unfuelled mass: 3,100 kg (6,800 lb). Specific impulse: 448 s. Burn time: 600 s. Height: 12.00 m (39.00 ft). Diameter: 3.35 m (10.99 ft). Span: 5.00 m (16.40 ft).

No Engines: 2.

Family: Space Tugs. Country: China. Engines: YF-75. Launch Vehicles: CZ-NGLV-320, CZ-NGLV-522/HO, CZ-NGLV-504/HO, CZ-NGLV-540/HO. Propellants: Lox/LH2.

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