Mass reduction of a conceptual microsatellite aluminum structure via employing perforation patterns

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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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Bibliographic Details
Main Author:	Dawood, Sarmad Dawood Salman
Format:	Thesis
Language:	English
Published:	2022
Subjects:	Aerospace engineering
Online Access:	http://psasir.upm.edu.my/id/eprint/114885/ http://psasir.upm.edu.my/id/eprint/114885/1/114885.pdf

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