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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Format: | Article |
Language: | English |
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Naval Academy Press
2019-06-01
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Series: | Scientific Bulletin of Naval Academy |
Subjects: | |
Online Access: | https://www.anmb.ro/buletinstiintific/buletine/2019_Issue1/01_MES/98.pdf |