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silicon carbide (SiC) fibres (monofilaments) are used in C/C or CMC composite materials (ceramic matrix composites) by the aerospace industry (brake discs, rocket engine nozzles, thrust chambers, leading
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key materials—generally nickel-based superalloys—that make up turbine blades with ceramic matrix composites (CMCs). These composites combine lightness, thermomechanical strength and damage tolerance
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-access research tool, allowing consultation and study of lexicographical material, as well as all the necessary sources and references. The ambition of the TGL-ReACH project is therefore to produce
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