TY - JOUR
T1 - Influence of SiC morphology and distribution on the ablation behavior of Ta0.8Hf0.2C-SiC coating for C/C composites
AU - Liu, Shaopu
AU - Wang, Yaxin
AU - Gu, Ping
AU - Ma, Zhuang
AU - Liu, Yanbo
AU - Tian, Xinchun
AU - Zhu, Shizhen
AU - Liu, Ling
N1 - Publisher Copyright:
© 2025 Elsevier Ltd
PY - 2026/2
Y1 - 2026/2
N2 - To enhance the ablation resistance of carbon/carbon (C/C) composites under extreme thermal environments, Ta0.8Hf0.2C-SiC coatings were fabricated via pack cementation, with the morphology and distribution of SiC precisely tuned by adjusting the fabrication temperature. The influence of SiC characteristics on coating microstructure, oxide evolution, and ablation behavior was systematically investigated. Coatings with optimally sized (∼30–40 μm), well-dispersed SiC exhibited the highest spectral emissivity (2.5–3 μm), enabling efficient thermal radiation and surface temperature reduction. During oxyacetylene ablation at 2130 ℃ for 300 s, the optimized coating formed a dense, low-volatility Ta-Hf-Si-O oxide layer and achieved a near-zero linear ablation rate (0.103 μm/s). In contrast, coatings with underdeveloped or overgrown SiC led to porous structures, phase segregation, and inferior thermal protection. This study demonstrates the key role of SiC morphology in controlling oxide phase evolution and provides a promising strategy for the design of advanced carbide-based coatings for ultra-high-temperature aerospace applications.
AB - To enhance the ablation resistance of carbon/carbon (C/C) composites under extreme thermal environments, Ta0.8Hf0.2C-SiC coatings were fabricated via pack cementation, with the morphology and distribution of SiC precisely tuned by adjusting the fabrication temperature. The influence of SiC characteristics on coating microstructure, oxide evolution, and ablation behavior was systematically investigated. Coatings with optimally sized (∼30–40 μm), well-dispersed SiC exhibited the highest spectral emissivity (2.5–3 μm), enabling efficient thermal radiation and surface temperature reduction. During oxyacetylene ablation at 2130 ℃ for 300 s, the optimized coating formed a dense, low-volatility Ta-Hf-Si-O oxide layer and achieved a near-zero linear ablation rate (0.103 μm/s). In contrast, coatings with underdeveloped or overgrown SiC led to porous structures, phase segregation, and inferior thermal protection. This study demonstrates the key role of SiC morphology in controlling oxide phase evolution and provides a promising strategy for the design of advanced carbide-based coatings for ultra-high-temperature aerospace applications.
KW - Ablation resistance
KW - Carbon/carbon composites
KW - TaHfC-SiC coating
KW - Ultra-high temperature ceramic
UR - http://www.scopus.com/pages/publications/105016464921
U2 - 10.1016/j.jeurceramsoc.2025.117834
DO - 10.1016/j.jeurceramsoc.2025.117834
M3 - Article
AN - SCOPUS:105016464921
SN - 0955-2219
VL - 46
JO - Journal of the European Ceramic Society
JF - Journal of the European Ceramic Society
IS - 2
M1 - 117834
ER -