Computational study of mass reduction of a conceptual microsatellite structural subassembly utilizing metal perforations

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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Bibliographic Details
Main Authors:	Salman Dawood, Sarmad Dawood, Harmin, Mohammad Yazdi, Mohd Harithuddin, Ahmad Salahuddin, Chia, Chen Ciang, Mohd Rafie, Azmin Shakrine
Format:	Article
Published:	The Aeronautical and Astronautical Society of the Republic of China 2021

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