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CZ-NGLV-KO
LOx/Kerosene propellant rocket stage. Upper stage for the 3.35 m diameter core vehicle. Only information available are the types of propellants, total thrust, and number of engines. Therefore all values shown here except thrust are estimated. This launcher has a low priority since its payload capability overlaps existing Chinese launch vehicles, and it would not be developed until after 2010.

Status: In development. Thrust: 588.00 kN (132,187 lbf). Gross mass: 60,000 kg (132,000 lb). Unfuelled mass: 7,000 kg (15,400 lb). Specific impulse: 340 s. Burn time: 300 s. Height: 13.00 m (42.00 ft). Diameter: 3.35 m (10.99 ft). Span: 3.35 m (10.99 ft).

No Engines: 4.



Country: China. Launch Vehicles: CZ-NGLV-320. Propellants: Lox/Kerosene.

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