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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




 
10/03/2017: Access of foreign journalists to the territory of SSAU subordinated enterprise

09/27/2017: SSAU Chairman Pavlo Degtiarenko participates in the International Astronautical Congress

09/22/2017: Chairman of the State Space Agency of Ukraine held a meeting with European experts within the framework of EGNOS program extension to Ukraine

09/14/2017: SSAU Chairman visited the "Ukrkosmos" SE

09/08/2017: SSAU Chairman held a meeting with Ambassador Extraordinary and Plenipotentiary of Canada to Ukraine