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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....
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| Gepubliceerd in: | Nat Commun |
|---|---|
| Hoofdauteurs: | , , , , , , , , |
| Formaat: | Artigo |
| Taal: | Inglês |
| Gepubliceerd in: |
Nature Publishing Group
2017
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| Onderwerpen: | |
| Online toegang: | https://ncbi.nlm.nih.gov/pmc/articles/PMC5474735/ https://ncbi.nlm.nih.gov/pubmed/28613275 https://ncbi.nlm.nih.govhttp://dx.doi.org/10.1038/ncomms15836 |
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