Designing of a solar panel deployment mechanism for small satellite
In the last few years, there has been a considerable increase of low cost space mission. Almost every small satellite has appendages like Solar Panels OR Antennas. These appendages have large inertial forces with low structural rigidity and mass to size ratio. These appendages are in stowed position...
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| Format: | Dissertation |
| Language: | English |
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Faculty of Engineering and the Built Environment
2021
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| Online Access: | http://hdl.handle.net/11427/33822 |