Thermal analysis of the 6U CubeSat Velox-II
Development and experimentation of small satellites have become feasible with the advancements in technologies in aerospace industries. The satellites are subjected to various types of thermal loads or radiative loads while in orbit. Every component of the spacecraft has its own temperature...
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| 格式: | Theses and Dissertations |
| 語言: | English |
| 出版: |
2015
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| 主題: | |
| 在線閱讀: | http://hdl.handle.net/10356/64807 |
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