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Ablation-resistant carbide Zr(0.8)Ti(0.2)C(0.74)B(0.26) for oxidizing environments up to 3,000 °C
Ultra-high temperature ceramics are desirable for applications in the hypersonic vehicle, rockets, re-entry spacecraft and defence sectors, but few materials can currently satisfy the associated high temperature ablation requirements. Here we design and fabricate a carbide (Zr(0.8)Ti(0.2)C(0.74)B(0....
Autores principales: | Zeng, Yi, Wang, Dini, Xiong, Xiang, Zhang, Xun, Withers, Philip J., Sun, Wei, Smith, Matthew, Bai, Mingwen, Xiao, Ping |
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Formato: | Online Artículo Texto |
Lenguaje: | English |
Publicado: |
Nature Publishing Group
2017
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Materias: | |
Acceso en línea: | https://www.ncbi.nlm.nih.gov/pmc/articles/PMC5474735/ https://www.ncbi.nlm.nih.gov/pubmed/28613275 http://dx.doi.org/10.1038/ncomms15836 |
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