Wenjing Luo , Hongting Tang , Rong Li , Bangbang Liu , Baojiong Hu , Qiang Zhen
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引用次数: 0
Abstract
Ultra-high-temperature ceramics (UHTCs), owing to their exceptional performance under extreme heat and harsh conditions, have become the preferred choice for critical thermal protection materials in high-speed aerospace vehicles. Here, the HfC-TiC ceramics were fabricated through pressureless sintering, and its oxidation behaivor was investigated using non-isothermal method. The oxidation activation energy of HfC-TiC sample reaches 385.39 kJ/mol. Then the ablation behavior of HfC-TiC ceramics was tested under plasma ablation conditions (3000 K, 5.0 MW/m2). The mass ablation rate and linear ablation rate of HfC-TiC can reach −1.11 × 10−3 g·s−1 and −1.40 × 10−3 mm·s−1 after being ablated for 300 seconds, respectively. The oxide layers in the center consisted of a porous oxide upper layer, a dense Ti-enriched intermediate layer, and an oxide inner layer. This complex multi-layered oxidative configuration synergistically protected the underlying carbide matrix, significantly enhancing the ablation resistance of HfC-TiC ceramics.
期刊介绍:
The Journal of the European Ceramic Society publishes the results of original research and reviews relating to ceramic materials. Papers of either an experimental or theoretical character will be welcomed on a fully international basis. The emphasis is on novel generic science concerning the relationships between processing, microstructure and properties of polycrystalline ceramics consolidated at high temperature. Papers may relate to any of the conventional categories of ceramic: structural, functional, traditional or composite. The central objective is to sustain a high standard of research quality by means of appropriate reviewing procedures.