Abstract
To address the demand for ablation-resistant materials suitable for applications in hypersonic vehicles operating in extreme environments, ultrahigh-temperature-ceramic–modified carbon/carbon composites (C/C-UHTCs) have emerged as a key research focus. In this study, we fabricate C/C-SiC-ZrC composites via reactive melt infiltration (RMI) and investigated the effects of different Si-Zr alloy compositions on the RMI mechanism and ablation behavior of the materials. Under identical conditions, an increase in the Zr concentration results in a decrease in the material density and a concomitant increase in the porosity. The elevated Zr concentration in the alloy modifies the element-diffusion mechanism during RMI, thus affecting the overall RMI process. Ablation experiments reveal that the samples fabricated with ZrSi2 and ZrSi via RMI exhibit similar ablation rates, which are significantly lower than that of the sample prepared with Zr2Si. This divergence stems from the formation of relatively uniform and dense ceramic layers on the surfaces of the samples obtained by the RMI of ZrSi2 and ZrSi, which provide protection during ablation. This study provides both theoretical and experimental backing for the fabrication and process optimization of C/C-ZrC-SiC composites prepared via RMI.
| Original language | English |
|---|---|
| Journal | Ceramics International |
| DOIs | |
| Publication status | Accepted/In press - 2026 |
| Externally published | Yes |
Keywords
- Ablation behavior
- C/C composites
- Matrix modification
- Reactive melt infiltration
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