The Hipparcos payload thermal control is presented. It ensures the active and passive thermal control with a temperature stability better than 0.05C over short periods, and about 2C over the entire mission duration. The payload structure, manufactured from carbon fiber reinforced plastic, is described. The principles of the active thermal control system are indicated, and its characteristics are listed.
Payload Thermal Control
1989
3 pages
Report
Keine Angabe
Englisch
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