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Carbon fiber reinforced ultra-high temperature ceramic matrix composites: A review
Affiliation:1. Katayanagi Advanced Research Laboratories, Tokyo University of Technology, 1404-1 Katakuramachi, Hachioji, Tokyo, 192-0982, Japan;2. Department of Materials Science & Technology, Tokyo University of Science, 6-3-1, Nijyuku, Katsushika-ku, Tokyo, 125-8585, Japan;3. Department of Space Flight Systems, Institute of Space and Astronautical Science (ISAS), Japan Aerospace Exploration Agency (JAXA), 3-1-1 Yoshinodai, Chuo-ku, Sagamihara, Kanagawa, 252-0222, Japan;1. CNR-ISTEC, Institute of Science and Technology for Ceramics, Via Granarolo 64, I-48018 Faenza, Italy;2. Department of Materials Science and Engineering, Missouri University of Science and Technology, Rolla, MO, 65409, United States;1. Department of Chemistry, University of Connecticut, 55 N. Eagleville Rd, Storrs, CT 06269, USA;2. Pratt & Whitney, East Hartford, CT 06118, USA;1. School of Metallurgy and Materials, University of Birmingham, B15 2SE, UK;2. MBDA, Le Plessis Robinson, 92350, France;3. MBDA, Stevenage, SG1 2DA, UK;4. DSTL, Salisbury, SP4 0JQ, UK;5. DGA, Bagneux, 92 221, France;1. Department of Materials Science & Technology, Tokyo University of Science, 6-3-1, Nijyuku, Katsushika-ku, Tokyo 125-8585, Japan;2. Katayanagi Advanced Research Laboratories, Tokyo University of Technology, 1404-1 Katakuramachi, Hachioji, Tokyo 192-0982, Japan;3. Aeronautical Technology Directorate,Japan Aerospace Exploration Agency (JAXA), Osawa 6-13-1, Mitaka-shi, Tokyo 181-0015, Japan;4. Department of Space Flight Systems, Institute of Space and Astronautical Science (ISAS), Japan Aerospace Exploration Agency (JAXA), 3-1-1 Yoshinodai, Chuo-ku, Sagamihara, Kanagawa 252-0222, Japan
Abstract:Recent studies on carbon fiber-reinforced ultra-high temperature ceramic matrix (C/UHTC) composites fabricated by hot-pressing, chemical vapor infiltration, polymer impregnation and pyrolysis, and melt infiltration (MI) are reviewed. Various efforts have been made to improve these preparation processes and to combine two or more of these because they have both the advantages and disadvantages in terms of the processing time, operating temperature, and the porosity of the resulting C/UHTC composites. In addition, the parameters governing the fracture toughness, thermal conductivity, and recession behavior (in oxidizing environments) of these composites have been discussed. This review demonstrates that C/UHTC composites with Zr- or Hf-based UHTC matrices fabricated via MI are potential candidates for advanced heat-resistant structural materials.
Keywords:Composites  Ultra high temperature ceramics (UHTCs)  Carbon fiber  Mechanical properties  Thermal properties  Thermal protection system
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