Mass reduction of a conceptual microsatellite aluminum structure via employing perforation patterns
Mass reduction is a primary design goal pursued in satellite structural design, since the launch cost is proportional to their total mass. The most common mass reduction method currently employed is to introduce honeycomb structures, with space qualified composite materials as facing materials, i...
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| Format: | Thesis |
| Language: | English |
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2022
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| Online Access: | http://psasir.upm.edu.my/id/eprint/114885/1/114885.pdf |