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Research paper | Publishing Language: Chinese | Open Access

Preparation of SiC/TiC composite ceramics by precursor conversion method and their oxy-propane ablation behavior at 1600 ℃

Yongbo CAO1,2Yulei ZHANG1,3( )Xinyi HU1,2Yanqin FU1Hejun LI3
Henan Key Laboratory of High Performance Carbon Fiber Reinforced Composites,Institute of Carbon Matrix Composites,Henan Academy of Sciences,Zhengzhou 450046,China
School of Materials Science and Engineering,Henan University of Science and Technology,Luoyang 471000,Henan,China
Shaanxi Engineering Research Center of Carbon/Carbon Composites,Science and Technology on Thermostructural Composite Materials Laboratory,Northwestern Polytechnical University,Xi’an 710072,China
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Abstract

To address the issues of volatile oxide scale and insufficient oxidation/ablation resistance of monolithic SiC ceramics in extreme environments, this study employs polysiloxane as a ceramic precursor and titanium acetylacetonate (TiO(acac)2) as a modifier. SiC/TiC composite ceramics are prepared via a precursor conversion method combined with spark plasma sintering. The cross-linking and curing mechanism of the precursor, as well as the high-temperature pyrolysis behavior, are systematically investigated, and the influence mechanism of Ti doping on the oxidation/ablation resistance of the composite ceramics is elucidated. The results show that Ti promotes precursor cross-linking through the formation of Si―O―Ti bonds, achieving a ceramic yield as high as 79.18%. When the TiO(acac)2 mass content reaches 20%, the TiC mass content in the composite increases to 19%, and the densification of the sintered ceramic is significantly improved. Oxy-propane ablation tests at 1600 ℃ demonstrate that the 20% modified sample exhibits greatly enhanced ablation resistance, with linear and mass ablation rates of 0.017 μm/s and −0.140 mg/s, respectively. This superior ablation resistance is attributed to the formation of a continuous composite oxide layer consisting of TiO2 and SiO2, which suppresses the volatilization of SiO2 and further oxygen diffusion.

CLC number: V254.2;TB332 Document code: A Article ID: 1007–7162(2026)9–97–10

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Journal of Aeronautical Materials
Pages 97-106

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Cite this article:
CAO Y, ZHANG Y, HU X, et al. Preparation of SiC/TiC composite ceramics by precursor conversion method and their oxy-propane ablation behavior at 1600 ℃. Journal of Aeronautical Materials, 2026, 46(9): 97-106. https://doi.org/10.11868/j.issn.1005-5053.2026.000073

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Received: 31 March 2026
Accepted: 29 April 2026
Published: 15 September 2026
© Journal of Aeronautical Materials 2026.

This is an open access article under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).