Ablation behavior of Hf-Zr-modified silicon-based ceramic coatings prepared by polymer derived ceramics and gaseous silicon infiltration

To improve the ablation resistance of C/C composite at temperatures exceeding 2000 °C, a (Hf-Zr)C-SiC Ultra-High Temperature Ceramic (UHTC) coating was prepared by Polymer Derived Ceramics (PDCs) and Gaseous Silicon Infiltration (GSI). The linear ablation rate of the coated C/C composites was as low as 0.27 μm/s, maintaining a level as low as 10 -4 mm/s. This low R l is attributed to the formation of a well-bonded double-layered oxide scale with high thermal stability, consisting of an exterior SiO 2 glass layer and an interior Hf-Zr-Si-O complex oxide layer. Meanwhile, the dissipation of the residual Si and the C phase relieves heat accumulation, ensuring that the recorded surface temperature remains below 2000 °C, thereby enhancing the ablation resistance. Additionally, a cyclic evolution of linear ablation rate was found, due to the alternating dominant role of oxidation and mechanical denudation on the coating during ablation. This study provides theoretical and experimental support for the long-term anti-ablation design of highly dense UHTC coatings.

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Publication Details

Journal
Chinese Journal of Aeronautics
Published
2025-12-12
DOI
https://doi.org/10.1016/j.cja.2025.104010
Primary Topic
Advanced ceramic materials synthesis
Type
article
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article

Ablation behavior of Hf-Zr-modified silicon-based ceramic coatings prepared by polymer derived ceramics and gaseous silicon infiltration

Laura Feldmann, Ralf Riedel, Yuqi Wang, Yue Dong et al.
Chinese Journal of Aeronautics
Advanced ceramic materials synthesis
article

Ablation behavior of Hf-Zr-modified silicon-based ceramic coatings prepared by polymer derived ceramics and gaseous silicon infiltration

Laura Feldmann, Ralf Riedel, Yuqi Wang, Yue Dong, Jia Sun, Lingxiang Guo, Shiwei HUANG
article en

Abstract

To improve the ablation resistance of C/C composite at temperatures exceeding 2000 °C, a (Hf-Zr)C-SiC Ultra-High Temperature Ceramic (UHTC) coating was prepared by Polymer Derived Ceramics (PDCs) and Gaseous Silicon Infiltration (GSI). The linear ablation rate of the coated C/C composites was as low as 0.27 μm/s, maintaining a level as low as 10 -4 mm/s. This low R l is attributed to the formation of a well-bonded double-layered oxide scale with high thermal stability, consisting of an exterior SiO 2 glass layer and an interior Hf-Zr-Si-O complex oxide layer. Meanwhile, the dissipation of the residual Si and the C phase relieves heat accumulation, ensuring that the recorded surface temperature remains below 2000 °C, thereby enhancing the ablation resistance. Additionally, a cyclic evolution of linear ablation rate was found, due to the alternating dominant role of oxidation and mechanical denudation on the coating during ablation. This study provides theoretical and experimental support for the long-term anti-ablation design of highly dense UHTC coatings.

Chinese Journal of AeronauticsVol. 39(5)
Openalex Percentile: Top 63%
Advanced ceramic materials synthesis
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Ablation behavior of Hf-Zr-modified silicon-based ceramic coatings prepared by polymer derived ceramics and gaseous silicon infiltration — Laura Feldmann, Ralf Riedel, et al. · Chinese Journal of Aeronautics (2025) | TGRS Research Map | TGRS