Design, analysis and optimization of a micro-satellite for the study of lower thermosphere and re-entry conditions
The scope of this thesis is to design, built and test a Double-Unit nanosatellite, with the view of launching and operate it in the lower thermosphere. The key innovative approach is the design optimization for an actual space mission, creating a hybrid design for the structural subsystem. The new d...
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| Άλλοι συγγραφείς: | |
| Μορφή: | Thesis |
| Γλώσσα: | English |
| Έκδοση: |
2017
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| Διαθέσιμο Online: | http://hdl.handle.net/10889/10553 |
