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Open Access

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

Lingxiang GUOaYaojun DONGbYuqi WANGaShiwei HUANGaLaura FELDMANNcRalf RIEDELcJia SUNa( )
Science and Technology on Thermostructural Composite Materials Laboratory, Northwestern Polytechnical University, Xi’an 710072, China
Science and Technology on Space Physics Laboratory, China Academy of Launch Vehicle Technology, Beijing 100076, China
Institute of Materials Science, Technical University of Darmstadt, Darmstadt D-64287, Germany

Peer review under responsibility of Editorial Committee of CJA.

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Abstract

To improve the ablation resistance of C/C composite at temperatures exceeding 2000 ℃, 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 Rl is attributed to the formation of a well-bonded double-layered oxide scale with high thermal stability, consisting of an exterior SiO2 glass layer and an interior Hf-Zr-Si-O complex oxide layer. Meanwhile, the dissipation of the residual Si and the C phases relieves heat accumulation, ensuring that the recorded surface temperature remains below 2000 ℃, 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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Chinese Journal of Aeronautics

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Cite this article:
GUO L, DONG Y, WANG Y, et al. Ablation behavior of Hf-Zr-modified silicon-based ceramic coatings prepared by polymer derived ceramics and gaseous silicon infiltration. Chinese Journal of Aeronautics, 2026, 39(5). https://doi.org/10.1016/j.cja.2025.104010

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Received: 24 February 2025
Revised: 03 April 2025
Accepted: 13 May 2025
Published: 12 December 2025
© 2025 The Authors. Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).