Computational study of mass reduction of a conceptual microsatellite structural subassembly utilizing metal perforations
A subassembly from the structural subsystem for a conceptual microsatellite designed for earth resources missions underwent normal modes analyses, after implementing an alternative approach to mass reduction, other than implementing advanced space qualified materials. This approach involved developi...
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| Format: | Article |
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The Aeronautical and Astronautical Society of the Republic of China
2021
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