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EPDM rubber insulation layer is used in solid rocket motor. Because aluminium trioxide particles will be produced after propellant combustion, it will produce heat and force effect on the insulation layer. In view of this situation, a thermo-mechanical coupling model for ablation of insulation is established.

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This page is a summary of: Ablation Model Based on Porous Charring Layer Under Alumina Erosion Condition, AIAA Journal, November 2019, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j058479.
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