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

  • Lingxiang GUO
  • , Yaojun DONG
  • , Yuqi WANG
  • , Shiwei HUANG
  • , Laura FELDMANN
  • , Ralf RIEDEL
  • , Jia SUN
  • Northwestern Polytechnical University Xian
  • China Aerospace Science and Technology Corporation
  • Technische Universität Darmstadt

Research output: Contribution to journalArticlepeer-review

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 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 °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.

Original languageEnglish
Article number104010
JournalChinese Journal of Aeronautics
Volume39
Issue number5
DOIs
StatePublished - May 2026

Keywords

  • Ablation resistance
  • C/C composites
  • Gaseous silicon infiltration
  • Multi-component carbide
  • Polymer derived ceramics

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