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....

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Detalles Bibliográficos
Autores principales: Zeng, Yi, Wang, Dini, Xiong, Xiang, Zhang, Xun, Withers, Philip J., Sun, Wei, Smith, Matthew, Bai, Mingwen, Xiao, Ping
Formato: Online Artículo Texto
Lenguaje:English
Publicado: Nature Publishing Group 2017
Materias:
Article
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

Internet

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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