Abstract
To prevent the ablation of carbon fiber reinforced carbon (C/C) composites from high temperature, a silicon carbide-hafnium silicide-tantalum disilicide (SiC-HfSi2-TaSi2) compound coating with high temperature anti-ablation ability was prepared on the surface of C/C composites by a calcining technique of pack cementation. The anti-ablation behavior of C/C composites was evaluated by an oxyacetylene flame. The morphologies, element distribution and phase composition of the surface and cross-sections of the SiC-HfSi2-TaSi2 coating before and after ablation were investigated by X-ray diffraction, scanning electron microscopy and energy dispersive spectroscopy. The results show that, because of the good stability of the HfO2 and Ta2O5 formed during ablation, the SiC-HfSi2-TaSi2 coating exhibits favorable anti-ablative properties. The linear ablation rate of C/C composites with the SiC-HfSi2-TaSi2 coating is 0.009 mm/s, and the mass ablation rate is 0.00385 g/s at 3000°C after ablation for 20 s.
| Original language | English |
|---|---|
| Pages (from-to) | 804-807 |
| Number of pages | 4 |
| Journal | Kuei Suan Jen Hsueh Pao/Journal of the Chinese Ceramic Society |
| Volume | 37 |
| Issue number | 5 |
| State | Published - May 2009 |
Keywords
- Anti-ablation
- Carbon fiber reinforced carbon composites
- Coating
- Silicon carbide-hafnium silicide-tantalum disilicide