Joining of ceramic matrix composites to high temperature ceramics for thermal protection systems

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dc.contributor.authorJiménez, C.
dc.contributor.authorMergia, K.
dc.contributor.authorLagos, M.A.
dc.contributor.authorYialouris, P.
dc.contributor.authorAgote, Iñigo
dc.contributor.authorLiedtke, V.
dc.contributor.authorMessoloras, S.
dc.contributor.authorPanayiotatos, Y.
dc.contributor.authorPadovano, E.
dc.contributor.authorBadini, C.
dc.contributor.authorWilhelmi, C.
dc.contributor.authorBárcena, Jorge
dc.contributor.institutionEXTREMAT
dc.date.issued2016-02-01
dc.descriptionPublisher Copyright: © 2015 Elsevier Ltd.
dc.description.abstractThe current work reports a novel approach for the integration of external protective SIC multilayers with ceramic matrix composite (C-f/SiC) with the view of application in aerospace heat protection systems. The integration method is based on diffusion brazing bonding. As a joining agent the MAX-Phase Ti3SiC2, produced by self-propagating high temperature synthesis, has been employed. The pressure applied during the joining process and its effect on the microstructure of the integrated structure is discussed. Microstructural analysis of the resulting joints is conducted using scanning electron microscopy coupled with energy dispersive spectroscopy and X-ray diffraction measurements. Analysis of the joints showed that the bonds are uniform, dense, with few crack vertical to the interface which are not detrimental for the performance of the joints. Ground re-entry tests showed that the joints survive 5 re-entry cycles at 1391 and 1794 degrees C without any detectable damage. (C) 2015 Elsevier Ltd. All rights reserved.en
dc.description.statusPeer reviewed
dc.format.extent7
dc.format.extent2708146
dc.identifier.citationJiménez , C , Mergia , K , Lagos , M A , Yialouris , P , Agote , I , Liedtke , V , Messoloras , S , Panayiotatos , Y , Padovano , E , Badini , C , Wilhelmi , C & Bárcena , J 2016 , ' Joining of ceramic matrix composites to high temperature ceramics for thermal protection systems ' , unknown , vol. unknown , no. 3 , pp. 443-449 . https://doi.org/10.1016/j.jeurceramsoc.2015.09.038
dc.identifier.doi10.1016/j.jeurceramsoc.2015.09.038
dc.identifier.otherresearchoutputwizard: 11556/110
dc.identifier.urlhttp://www.scopus.com/inward/record.url?scp=84955574762&partnerID=8YFLogxK
dc.language.isoeng
dc.relation.ispartofunknown
dc.rightsinfo:eu-repo/semantics/restrictedAccess
dc.subject.keywordsCeramic matrix composites
dc.subject.keywordsSilicon carbide
dc.subject.keywordsJoining
dc.subject.keywordsThermal tests
dc.subject.keywordsAerospace
dc.subject.keywordsCeramic matrix composites
dc.subject.keywordsSilicon carbide
dc.subject.keywordsJoining
dc.subject.keywordsThermal tests
dc.subject.keywordsAerospace
dc.subject.keywordsCeramic matrix composite
dc.subject.keywordsCeramics and Composites
dc.subject.keywordsMaterials Chemistry
dc.subject.keywordsProject ID
dc.subject.keywordsinfo:eu-repo/grantAgreement/EC/FP7/262749/EU/MULTIFUNCTIONAL COMPONENTS FOR AGRESSIVE ENVIROMENTS IN SPACE APPLICATIONS/SMARTEES
dc.subject.keywordsinfo:eu-repo/grantAgreement/EC/FP7/262749/EU/MULTIFUNCTIONAL COMPONENTS FOR AGRESSIVE ENVIROMENTS IN SPACE APPLICATIONS/SMARTEES
dc.subject.keywordsFunding Info
dc.subject.keywordsEuropean Project "SMARTEES (G.A.) 262749, European Community
dc.subject.keywordsEuropean Project "SMARTEES (G.A.) 262749, European Community
dc.titleJoining of ceramic matrix composites to high temperature ceramics for thermal protection systemsen
dc.typejournal article
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