Nanosat power system planning and analysis
碩士 === 國立中央大學 === 機械工程研究所 === 90 === The goal of this thesis is design a power system to fit the Nanosat use to reach the mission requirement. The weight of Nanosat is 10 kilograms, sun-synchronous circular orbit, orbit altitude is 800 km, orbit inclination is 98.6 degree, orbit period is 101 minut...
| Main Authors: | , |
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| Format: | Others |
| Language: | zh-TW |
| Published: |
2002
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| Online Access: | http://ndltd.ncl.edu.tw/handle/50272426659053957996 |