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Research progress on reusable ultra−high temperature ceramic matrix composites
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Fuchen LIU1, 2, Bowen CHEN1, *, Dewei NI1, Yan GU1, Ling LIN1, Feiyan CAI1, Yusheng DING1, Shaoming DONG1, *
Science & Technology Review | 2026, 44(13) : 64 - 78
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Science & Technology Review | 2026, 44(13): 64-78
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Research progress on reusable ultra−high temperature ceramic matrix composites
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Fuchen LIU1, 2, Bowen CHEN1, *, Dewei NI1, Yan GU1, Ling LIN1, Feiyan CAI1, Yusheng DING1, Shaoming DONG1, *
Affiliations
  • 1Center of Structural Ceramics and Composite Materials, Shanghai Institute of Ceramics, Chinese Academy of Sciences, Shanghai 201899, China
  • 2College of Materials Science and Opto−Electronic Technology, University of Chinese Academy of Sciences, Beijing 100049, China
Published: 2026-07-13 doi: 10.3981/j.issn.1000-7857.2025.12.00012
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Aerospace vehicles are rapidly evolving towards higher speeds, reusability, and lighter weight. Consequently, thermal protection systems face severe challenges, including extreme temperatures, repeated ablation, and mechanical loads. Ultra−high temperature ceramic matrix composites (UHTCMCs) are regarded as an ideal material for next−generation reusable thermal protection, due to key advantages such as high melting point, excellent ablation resistance, low density, high strength, and high reliability. This paper systematically reviews the main categories of thermal protection materials for aerospace vehicles and analyzes the performance requirements for reusable systems. The discussion focuses on recent research progress in the most promising UHTCMCs, particularly regarding resistance to repeated ablation. Key aspects covered include material composition design and optimization, fiber and interface tailoring, lightweight and integrated structure−function design, and advanced fabrication processes. Studies indicate that the repeated ablation resistance and structural reliability of UHTCMCs have been significantly improved. These advances result from composition optimization methods−such as multi−phase compounding, rare−earth modification, and high−entropy design−combined with innovative fiber and interface engineering. Looking ahead, further research should address several key challenges: understanding performance degradation under long−term cyclic thermal−mechanical coupling, enhancing the durability of fibers and interfaces in oxidative environments, developing life prediction and assessment methods, and advancing low−cost, efficient manufacturing. Cross−scale mechanistic studies and engineering application efforts in these areas are essential to enable the practical use of UHTCMCs in advanced reusable aerospace vehicles.

ultra−high temperature ceramic matrix composites (UHTCMCs)  /  reusability  /  aerospace vehicles  /  thermal protection system
Fuchen LIU, Bowen CHEN, Dewei NI, Yan GU, Ling LIN, Feiyan CAI, Yusheng DING, Shaoming DONG. Research progress on reusable ultra−high temperature ceramic matrix composites[J]. Science & Technology Review, 2026 , 44 (13) : 64 -78 . DOI: 10.3981/j.issn.1000-7857.2025.12.00012
Year 2026 volume 44 Issue 13
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doi: 10.3981/j.issn.1000-7857.2025.12.00012
  • Receive Date:2025-12-01
  • Online Date:2026-07-27
  • Published:2026-07-13
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  • Received:2025-12-01
  • Revised:2026-02-05
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Affiliations
    1Center of Structural Ceramics and Composite Materials, Shanghai Institute of Ceramics, Chinese Academy of Sciences, Shanghai 201899, China
    2College of Materials Science and Opto−Electronic Technology, University of Chinese Academy of Sciences, Beijing 100049, China
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表12种不同金属材料的力学参数

Family
属数
Number of
genus
种数
Number of
species
占总种数比例
Percentage of
total species (%)

Genus
种数
Number of
species
占总种数比例
Percentage of total
species (%)
鹅膏菌科Amanitaceae 2 11 5.26 鹅膏菌属 Amanita 10 4.78
小菇科 Mycenaceae 2 12 5.74 丝盖伞属 Inocybe 5 2.39
多孔菌科 Polyporaceae 8 14 6.70 蜡蘑属 Laccaria 5 2.39
红菇科 Russulaceae 3 23 11.00 小皮伞属 Marasmius 6 2.87
小菇属 Mycena 11 5.26
光柄菇属 Pluteus 5 2.39
红菇属 Russula 17 8.13
栓菌属 Trametes 5 2.39
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