KazEOSat 1 (DZZ-HR, HRES) |
Kazakhstan |
Spacecraft nº: |
Kazakhstan spacecraft nº: 4 |
Launch data:
|
Prime manufacturer | EADS Astrium ––> Airbus Defence and Space |
Platform | Leostar-500-XO |
Operator | Kazakhstan Gharysh Sapary (KGS) |
Mass at launch | 830 kg |
Dry Mass | kg |
Basic shape | |
Dimension (m) | |
Equipment | |
Solar array | Deployable fixed solar arrays |
Stabilization | |
Propulsion | Hydrazine thrusters |
DC power | |
Design lifetime | 7 yrs |
Ref.: #7(JR697), #14, #110, #228 - update: 02.12.14 | Home |