A new design proposal and thermal analysis of subassemblies inside a satellite

In this study, the authors aim to validate the use of CFRP composites in a subassembly of a satellite as a replacement for currently used aluminum. Considering the high costs of sending a mass unit of payload into orbit, the mass should be minimized. Therefore, the application of composite materia...

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Bibliographic Details
Main Author: Sorin Drăghici
Format: Article
Language:English
Published: Naval Academy Press 2019-06-01
Series:Scientific Bulletin of Naval Academy
Subjects:
Online Access:https://www.anmb.ro/buletinstiintific/buletine/2019_Issue1/01_MES/98.pdf