Abstract
The integrated molding of the coating and modified matrix was achieved by the precursor impregnation and pyrolysis (PIP) method. The average mass ablation rate of the prepared SiCnw-(ZrC-SiC) integrated coating on modified C/C composite material is only 0.60 mg/s after 5 × 120 s of ablation. The coating on the surface of the material is just exfoliated after 3 cycles of ablation. Additionally, there is still a protective layer formed by ZrO2-SiO2 on the surface of the matrix after 5 cycles of ablation. The results demonstrate that the integrated coating/matrix-modification is successful in enhancing thermal shock resistance and prolonging ablation life of the material.
| Original language | English |
|---|---|
| Pages (from-to) | 40431-40440 |
| Number of pages | 10 |
| Journal | Ceramics International |
| Volume | 51 |
| Issue number | 23 |
| DOIs | |
| State | Published - Sep 2025 |
Keywords
- Ablation
- C/C composite
- Coating
- Matrix modification
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