Integrated structural design optimization of space vehicles with multidisciplinary constraints

•A novel multidisciplinary design optimization framework for composite spacecraft structures, leveraging a combination of commercial and open-source tools to facilitate easy industry implementation.•Integration of Structures, Thermal and Acoustic disciplines with various static and dynamic loading e...

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Veröffentlicht in:	Aerospace science and technology Jg. 168; S. 110906
Hauptverfasser:	Borwankar, Pranav, Kapania, Rakesh K., Inoyama, Daisaku, Stoumbos, Tom
Format:	Journal Article
Sprache:	Englisch
Veröffentlicht:	Elsevier Masson SAS 01.01.2026
Schlagworte:	Acoustic analysis Composite structures Integer programming Lamination parameters MDO Spacecraft structures Thermal analysis Integer programming Lamination parameters MDO Spacecraft structures Thermal analysis Composite structures Acoustic analysis
ISSN:	1270-9638
Online-Zugang:	Volltext
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