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CZ-NGLV-500
LOx/LH2 propellant rocket stage. From top to bottom the 5-m Chinese new generation launch vehicle consists of a 117.3 cubic meter liquid oxygen tank, an intertank section, a 350.7 cubic meter liquid hydrogen tank, and an engine section with two gimbaled LOX /LH2 engines of 660 kN vacuum thrust each. The hydrogen tank is pressurized using hydrogen bled from the engine and helium is used to pressurize the oxygen tank.

Status: In development. Thrust: 1,399.99 kN (314,730 lbf). Gross mass: 175,000 kg (385,000 lb). Unfuelled mass: 17,000 kg (37,000 lb). Specific impulse: 432 s. Specific impulse sea level: 333 s. Burn time: 480 s. Height: 31.00 m (101.00 ft). Diameter: 5.00 m (16.40 ft). Span: 5.00 m (16.40 ft).

No Engines: 2.



Country: China. Engines: YF-50t. Launch Vehicles: CZ-NGLV-540, CZ-NGLV-522, CZ-NGLV-522/HO, CZ-NGLV-504, CZ-NGLV-504/HO, CZ-NGLV-540/HO. Propellants: Lox/LH2.

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