Preparation of carbon/carbon‐ultra high temperature ceramics composites with ultra high temperature ceramics coating-Reference-Cited by-同舟云学术

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Preparation of carbon/carbon‐ultra high temperature ceramics composites with ultra high temperature ceramics coating

Published:2018-04-03 Issue:9 Volume:101 Page:3830-3836
ISSN:0002-7820
Container-title:Journal of the American Ceramic Society
language:en
Short-container-title:J Am Ceram Soc

Author:

Xu Lin¹²^ORCID,Cheng Jia¹,Li Xingchao¹,Zhang Yin¹,Fan Zhen¹,Song Yongzhong¹,Feng Zhihai¹

Affiliation:

1. Science and Technology of Advanced Functional Composite Laboratory Aerospace Research Institute of Materials & Processing Technology Beijing China

2. Science and Technology on High Strength Structure Materials Laboratory Central South University Changsha China

Funder

Open Research Fund of Science and Technology on High Strength Structure Materials Laboratory

National Basic Research Program of China

Publisher

Wiley

Subject

Materials Chemistry,Ceramics and Composites

Link

https://onlinelibrary.wiley.com/doi/pdf/10.1111/jace.15565

Reference26 articles.

1. SchmidtDL.Carbon/carbon composites (CCC) ‐ a historical perspective. Technical Report;1996: WL‐TR‐96‐4107.

2. GlassDE DirlingR CroopH FryTJ FrankGJ.Materials development for hypersonic flight vehicles.14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference American Institute of Aeronautics and Astronautics;2006: AIAA‐2006‐81226.

3. GlassDE.Ceramic matrix composite (CMC) thermal protection systems (TPS) and hot structures for hypersonic vehicles.15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference American Institute of Aeronautics and Astronautics;2008: AIAA‐2008‐2682.

4. UHTC composites for hypersonic applications;Paul A;Am Ceram Soc Bull,2012

5. Fabrication and Characterization of an Ultra-High-Temperature Carbon Fiber-Reinforced ZrB2?SiC Matrix Composite

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