CZ-NGLV-KO
Stage · China
Original archive entry. The text, images and links below are kept as they were written.
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.
No Engines: 4.
Related
- Country
- China
- Launch Vehicles
- CZ-NGLV-320
- Propellants
- Lox/Kerosene