KazEOSat 1 (DZZ-HR, HRES) |
Kazakhstan |
Spacecraft nº: |
Kazakhstan spacecraft nº: 4 |
Launch data:
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| 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 |