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Volumn 4, Issue 1, 2008, Pages 53-62
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Thermal fatigue analysis of solar panel structure for micro-satellite applications
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Author keywords
Aerospace; Composite; Fatigue; Finite difference; Finite element; Honeycomb; Laminates; Satellite; Structure; Thermal
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Indexed keywords
FINITE DIFFERENCE METHOD;
FINITE ELEMENT METHOD;
HONEYCOMB STRUCTURES;
LAMINATED COMPOSITES;
STRUCTURAL PANELS;
THERMAL FATIGUE;
MICRO-SATELLITE APPLICATIONS;
SOLAR PANEL STRUCTURE;
SATELLITES;
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EID: 40249110650
PISSN: 15691713
EISSN: None
Source Type: Journal
DOI: 10.1007/s10999-008-9057-3 Document Type: Article |
Times cited : (12)
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References (22)
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