Flight test results of the passive cooling system
Abstract
An onboard power cooler model is described. The flight test results for three years are given. It is shown that during the radiator exposure, of the cooler external stage to Sun, for about 15 minutesat each orbit, and at the maximum angle of the Sunascension, less than 30 degrees, the radiator temperature of the radiator detector is 105 K.
- Publication:
-
ESA Special Publication
- Pub Date:
- December 1991
- Bibcode:
- 1991secs.conf..957A
- Keywords:
-
- Cooling Systems;
- Flight Tests;
- Radiators;
- Spacecraft Radiators;
- Spacecraft Temperature;
- Temperature Control;
- Cryogenics;
- Postflight Analysis;
- Temperature Measurement;
- Spacecraft Design, Testing and Performance