Heat dissipation of carbon shell in ZrC–SiC/TaC coating to improve protective ability against ultrahigh temperature ablation
Structural material
Carbon fibers
DOI:
10.26599/jac.2024.9220921
Publication Date:
2024-06-04T08:33:17Z
AUTHORS (6)
ABSTRACT
To efficiently decrease the ablation heat accumulation and improve protective ability of ZrC-SiC/TaC coating on carbon/carbon composites, a thermally conductive nano-network with ceramic@carbon core-shell structure was designed constructed. Polymer-derived SiC/TaC graphene carbon shell synthesized introduced into ZrC by supersonic atmospheric plasma spraying. Graphene paths were benefitted in increasing transfer capability lowering surface temperature about 200 °C during oxyacetylene ablation. The dissipation ZrC-SiC/TaC@C reduced volatilization low-melting-point phases delayed sintering ZrO<sub>2</sub> particles. Thus, decreased mass linear rates 91.4 % 93.7 compared to coating, respectively. This work provided constructive idea resistance coatings incorporating nanomaterials function dissipation.
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