Abstract

In this study, the UHTC-based composite layers where applied on the graphite substrates using SPS method to protect them against ablation. The protective layers had some defects and problems such as crack, fracture, separation, melting, and weak adhesion to the substrate. Several factors such as the thickness of composite layer, the number of protective layers, the SPS conditions (temperature, applied pressure, soaking time and mold), the chemical composition of the layers, the type of the substrate and the mismatch between the thermal expansion coefficients of the substrate and the applied layer(s) affected the quality and connection of the protective layer to the graphite substrate. The amount of additive materials influenced the melting phenomenon in the composite layer; for example, further MoSi2 in the layer led to more melting. The mismatch between the thermal expansion coefficients of the graphite substrate and the composite layer caused stresses during the cooling step, which resulted in cracks in the applied layer. Hence, proximity in the thermal expansion coefficients seems to be necessary for the formation of an acceptable adhesion between the layer and the substrate.

Highlights

  • Carbon materials and carbon-carbon composites are important materials in various industries like supersonic spacecraft, furnace elements, turbine blades, rocket nozzles, and space shuttle noses

  • Cracks and separations can be observed on the surface of the composite layer

  • Such defects are mainly caused by stresses during cooling rapid cooling of the sample due to the mismatch of the thermal expansion coefficients of the graphite substrate with the ultrahigh temperature ceramics (UHTCs)-based composite layers

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Summary

Introduction

Carbon materials and carbon-carbon composites are important materials in various industries like supersonic spacecraft, furnace elements, turbine blades, rocket nozzles, and space shuttle noses. These materials are promising candidates for high temperature usages where high strength and resistance to wear are demanded [1,2,3,4,5,6]. Ultrahigh temperature ceramics (UHTCs) are utilized as coatings on the graphite, owing to their unique properties such as high melting temperature (above 3000 °C), excellent resistance to oxidation, and unique mechanical properties [18,19,20]. Applying UHTCs coating on carboncarbon composites to inhibit oxidation can be an acceptable approach to design the heat protection systems if it has followings [24]: -Stability and integration to provide erosion resistance and limit evaporation. -Ability to stop oxygen penetration into the substrate. -Compatibility for resistance against lamination due to mismatch between the thermal expansion coefficients. -Simple manufacturability and reproducibility

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