thermal analyses and verification for hausat-2 small satellite
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ID: 204955
2006
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Abstract
HAUSAT-2 is nano satellite with 25 kg mass being developed by Space System Research Lab. in Hnakuk Aviation University. This paper addresses HAUSAT-2 small satellite thermal analyses and its verification at satellite system, electronic box, and PCB levels. Thermal model which is used for system-level and box-level thermal analyses was verified and corrected through thermal vacuum/balance test. The new board-level thermal analysis methodology, modelling high-power dissipating EEE parts directly, was proposed. The proposed methodology has been verified with test results.
| Reference Key |
lee2006journalthermal
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|---|---|
| Authors | ;Mi-Hyeon Lee;Dong-Woon Kim;Young-Keun Chang |
| Journal | the journal of supercritical fluids |
| Year | 2006 |
| DOI |
10.5140/JASS.2006.23.1.039
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