Construction of gradient structure C/C–ZrC–SiC composites with good ablation resistance

Author:

Wang Running,Zhang Jiaping,Fei Jie,Fu Qiangang

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Reference53 articles.

1. Radiation heat transfer during hypersonic flight: a review of emissivity measurement and enhancement approaches of ultra‐high temperature ceramics;Saad;Int J Ceram Eng Sci.,2023

2. Ultra-high temperature ceramics for extreme environments;Wyatt;Nat. Rev. Mater.,2023

3. Thermo-structural design of ZrB2-SiC-based thermal protection system for hypersonic space vehicles;Purwar;J. Am. Ceram. Soc.,2017

4. A systematic approach for horizontal and vertical scale up of sintered Ultra-High Temperature Ceramic Matrix Composites for aerospace–Advances and perspectives;Sciti;Compos. B Eng.,2022

5. Effect of annealing treatments on the mechanical behaviour of UHTCMCs prepared by mild polymer infiltration and pyrolysis;Servadei;Ceram. Int.,2023

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