| 77 | |
| 78 | The thermal control of the spacecraft is intended to be passive as far as possible. The sun-pointing attitude |
| 79 | results however in a considerable thermal gradient through the spacecraft, making as such a completely |
| 80 | passive thermal control difficult to achieve and heaters are foreseen to control the battery temperature. Heaters |
| 81 | are also required to de-contaminate specific parts of the solar observation instruments. The SWAP instrument |
| 82 | (see below) has a radiator mounted on the side of the spacecraft in order to keep the detector as cold as |
| 83 | possible. |
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| 85 | [wiki:File:PROBA2_Auto14.jpeg File:PROBA2 Auto14.jpeg] |
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