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Research Article | Open Access

Elevated temperature performance: Arc-jet testing of carbon fiber reinforced ZrB2 bars up to 2200 °C for strength retention assessment

D. Sciti1A. Vinci1( )L. Zoli1P. Galizia1M. Mor1W. Fahrenholtz2S. Mungiguerra3R. Savino3A. M. Caporale4A. Airoldi4
CNR-ISSMC, National Research Council of Italy - Institute of Science, Technology and Sustainability for Ceramics, Faenza 48018, Italy
Department of Materials Science and Engineering, Missouri University of Science and Technology, Rolla 65409-0330, USA
University of Naples, Dept. of Industrial Engineering, Naples 80125, Italy
Politecnico di Milano, Department of Aerospace Science and Technology, Milan 20156, Italy
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Abstract

For the first time, ultra-high temperature ceramic matrix composite bars were tested inside an arc-jet facility to investigate the impact of oxidation damage on strength retention. The composite bars, which were based on a ZrB2/SiC matrix reinforced with 45 vol% carbon fibers, were produced by slurry impregnation and sintering. The first batch was tested under 3-point (pt) bending, and two additional batches were exposed to plasma of dissociated air up to a temperature of 2200 °C for 2 min or 2.2 min and then subjected to 3-pt bending. More than 75% of the initial strength was retained even after repeated testing, demonstrating the durability and reusability of the material. Volatility diagrams were calculated to explain the oxide layering observed, while a numerical model was developed to correlate the experimental mechanical data with the elastic properties. The decrease of strength was attributed to a reduction of the cross section due to oxidation.

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Journal of Advanced Ceramics
Article number: 9221022

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Cite this article:
Sciti D, Vinci A, Zoli L, et al. Elevated temperature performance: Arc-jet testing of carbon fiber reinforced ZrB2 bars up to 2200 °C for strength retention assessment. Journal of Advanced Ceramics, 2025, 14(2): 9221022. https://doi.org/10.26599/JAC.2024.9221022

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Received: 17 September 2024
Revised: 18 December 2024
Accepted: 18 December 2024
Published: 26 February 2025
© The Author(s) 2025.

This is an open access article under the terms of the Creative Commons Attribution 4.0 International License (CC BY 4.0, http://creativecommons.org/licenses/by/4.0/).