MetOp-A |
ESA |
Spacecraft nº: |
ESA spacecraft nº: 62 |
Launch data:
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| Prime contractor | |
| Operator | |
| Platform | |
| Mass at launch | 4093 kg, including 316 kg hydrazine in 4 tanks |
| Dry Mass | kg |
| Basic shape | |
| Dimension (m) | 6.2m (high) by 3.4 x 3
m cross-section in launch configuration 17.6 x 6.5 x 5.2 m with solar array and antennas deployed |
| Solar array | 1 deployable Solar Array |
| Altitude control | 3-axis stabilised by reaction wheels; orbit manoeuvres by hydrazine thrusters; pointing knowledge 0.07° X-axis, 0.11° Y-axis, 0.15° Z-axis |
| DC power | |
| Design lifetime | 5 years |
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