Abstract
Given the diverse requirements of thermal protection systems for C/C composites, achieving a simultaneous enhancement of ablative and mechanical properties while ensuring lightweight is a great challenge. Recent research has discovered the development of a gradient structure has the potential to achieve multiple performance improvements simultaneously. Herein, we designed gradient C/C-ZrC-SiC composites by reactive melt infiltration and chemical vapor infiltration. The gradient structured C/C-ZrC-SiC composites achieve good shear strength of 62 MPa, revealing an increase of 26.3 % compared to the traditional C/C-ZrC-SiC composites. After ablation at 3000 °C for 60 s, the composites also show good ablation properties with linear and mass ablation rates of 2.37 μm/s and 2.07 mg/s, respectively, which is attributed to the synergistic effect of oxygen resistance of the dense oxide layer and heat transfer of the pyrolytic carbon network in gradient structure.
| Original language | English |
|---|---|
| Pages (from-to) | 17774-17785 |
| Number of pages | 12 |
| Journal | Ceramics International |
| Volume | 51 |
| Issue number | 13 |
| DOIs | |
| State | Published - May 2025 |
Keywords
- Ablation resistance
- C/C composites
- Gradient structure
- Mechanical property
- ZrC-SiC
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