Abstract
Protective coatings are indispensable for thermal protection systems, but damage during installation and service is often unavoidable. To restore the protective function of C/C–SiC–ZrC composites, an on-site repair strategy was developed using a non-sintered repair coating composed of polysilazane and HfSi2 particles. According to GJB323A-96 Standard with heat fluxes of 2.38 MW/m2, the ablation tests were investigated. Short-term exposure (10 s) induced the rapid oxidation of HfSi2, forming a dense HfO2 layer that sealed the surface and effectively hindered oxygen ingress. After 120 s, the repaired samples showed negative linear and mass ablation rates (−0.99 ± 0.07 μm/s and −0.50 ± 0.05 mg/s, respectively), indicating that the repaired coating still provided effective protection for the substrate. In contrast, uncoated composites suffered severe ablation with rates of 0.80 ± 0.17 μm/s and 1.00 ± 0.08 mg/s. Notably, the ablation rate of the repair coating was comparable to that of the in-situ coating, confirming the effectiveness of the proposed on-site repair strategy. Meanwhile, the HfSi2–HfO2 repair coating prepared through compositional and structural optimization further reduced the discrepancy between linear and mass ablation rates, confirming the effectiveness and reproducibility of the repair strategy.
| Original language | English |
|---|---|
| Pages (from-to) | 65537-65550 |
| Number of pages | 14 |
| Journal | Ceramics International |
| Volume | 51 |
| Issue number | 30 |
| DOIs | |
| State | Published - Dec 2025 |
Keywords
- Ablation resistance
- C/C-ZrC-SiC composites
- HfSiand HfSi–HfOrepair coatings
- On-site repair coatings
- Oxyacetylene flame test
- Reactive melt infiltration (RMI)
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