Thermal-Mechanical Optimization of Folded Core Sandwich Panels for Thermal Protection Systems of Space Vehicles

<div>Buckling modes of the ITPS panel. (a) Web buckling when TFS reaches maximum temperature. (b) Web buckling when web middle reaches maximum temperature. (c) Web buckling when BFS reaches maximum temperature.</div>

International Journal of Aerospace Engineering

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Figure 16

Figure 16: Thermal-Mechanical Optimization of Folded Core Sandwich Panels for Thermal Protection Systems of Space Vehicles 