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Cyclone-3



Design works on Cyclone-3 launch vehicle on the basis of Cyclone-2 rocket were started in 1970.

Cyclone-3 launch vehicle inherited high reliability and automation of pre-launch and launch operations from its Cyclone-2 ancestor.


Cyclone launcher main features:
      Launch vehicle
Cyclone 3
      Launch mass, tonnes
187
      Number of stages
3
      Maximal payload mass, tonnes:

      LEO

      GTO

3,6

0,6

      Launch azimuth, degrees
73-83
      Main fairing

      diameter, m

      height, m

2,7

9,5




 
12/19/2017: SSAU Chairman Pavlo Degtiarenko paid a working visit to the Kingdom of the Netherlands

12/12/2017: SSAU Chairman Pavlo Degtiarenko paid a working visit to Paris on December 11-12, 2017

12/07/2017: The working meeting of SSAU Chairman Pavlo Degtiarenko with Administrator of Chinese National Space Administration Mr. Tang Dengjie