Design and Test of The Power Subsystem For A Nanosat
碩士 === 淡江大學 === 機械與機電工程學系 === 91 === This thesis concerns about the hardware design and analysis of the power subsystem of Nanosat. The initial mission of Nanosat is atmosphere observation. It is a satellite under 10 kg, and adopts sun-synchronous orbit. The orbit altitude of Nanosat is 8...
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| Format: | Others |
| Language: | zh-TW |
| Published: |
2003
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| Online Access: | http://ndltd.ncl.edu.tw/handle/25160461260914140617 |