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Experimental study demonstrates enhanced tensile strength and reduced ablation rates in silicone composites, indicating potential for aerospace thermal protection.
This work develops a series of flexible thermal ablation‐resistant epoxy‐modified polydimethylsiloxane (EDA@PDMS) composites with integrated mechanical and thermal protection performance through multiscale design strategy. EDA@PDMS was prepared by epoxy ring‐opening and hydrosilylation reactions. Then, 10 phr silicon dioxide and 6 phr carbon fibers were added to simultaneously enhance the mechanical strength and ablation resistance of EDA@PDMS‐c. Results showed that the tensile strength of EDA@PDMS‐c reached 2.31 MPa, which is 41.7% higher than that of PDMS‐c. Under 4 MW/m 2 for 30 s, the linear ablation rate (LAR) and mass ablation rate (MAR) of EDA@PDMS‐c reached 0.0515 mm/s and 0.0357 g/s, which were 32.1% and 18.5% lower than those of PDMS‐c, respectively. Additionally, a peak back‐face temperature of 89.4°C was monitored during the ablation process, indicating excellent thermal insulation performance. The above improvement was ascribed to the combined effects of the intrigue molecular structure design through CSi synergistic mechanism and reinforcing fillers. The research proposed a strategy for fabricating high‐performance flexible ablation composites that can be potentially used for thermal protection purposes in the areas of fire protection and aerospace among others.
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Pan et al. (2026) studied this question.
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