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dc.contributor.authorTriantou, K.I.
dc.contributor.authorMergia, K.
dc.contributor.authorPerez, B.
dc.contributor.authorFlorez, S.
dc.contributor.authorStefan, A.
dc.contributor.authorBan, C.
dc.contributor.authorPelin, G.
dc.contributor.authorIonescu, G.
dc.contributor.authorZuber, C.
dc.contributor.authorFischer, W.P.P.
dc.contributor.authorBarcena, J.
dc.date.accessioned2017-03-07T15:29:07Z
dc.date.available2017-03-07T15:29:07Z
dc.date.issued2017-02
dc.identifier.citationK.I. Triantou, K. Mergia, B. Perez, S. Florez, A. Stefan, C. Ban, G. Pelin, G. Ionescu, C. Zuber, W.P.P. Fischer, J. Barcena, Thermal shock performance of carbon-bonded carbon fiber composite and ceramic matrix composite joints for thermal protection re-entry applications, Composites Part B: Engineering, Volume 111, 15 February 2017, Pages 270-278, ISSN 1359-8368, http://dx.doi.org/10.1016/j.compositesb.2016.12.020.en
dc.identifier.issn1359-8368en
dc.identifier.urihttp://hdl.handle.net/11556/373
dc.description.abstractHybrid thermal protection systems for aerospace applications based on carbon-bonded carbon fiber composite (CALCARB®) and ceramic matrix composites have been investigated. Two types of ceramic composite materials were considered, Cf/SiC (SiCARBON™) and C/C-SiC. The ablative material and the ceramic matrix composite were joined using alumina, graphite and zirconia-zirconium silicate based commercial high temperature adhesives and their performance on thermal shock tests was evaluated. Microstructural analysis of the joints after thermal shock tests was conducted using optical microscopy and scanning electron microscopy (SEM) coupled with energy dispersive spectroscopy (EDS). Both material combinations survive the thermal shock tests for the structures in which zirconia-zirconium silicate and graphite based adhesives were employed.en
dc.description.sponsorshipEuropean Project ‘‘HYDRA’’ (G.A. n. 283797) with the financial support by the European Commission.en
dc.language.isoengen
dc.publisherELSEVIER SCI LTD, THE BOULEVARD, LANGFORD LANE, KIDLINGTON, OXFORD OX5 1GB, OXON, ENGLANDen
dc.titleThermal shock performance of carbon-bonded carbon fiber composite and ceramic matrix composite joints for thermal protection re-entry applicationsen
dc.typearticleen
dc.identifier.doi10.1016/j.compositesb.2016.12.020en
dc.isiYesen
dc.relation.projectIDinfo:eu-repo/grantAgreement/EC/FP7/283797/EU/HYBRID ABLATIVE DEVELOPMENT FOR RE-ENTRY IN PLANETARY ATMOSPHERIC THERMAL PROTECTION/HYDRAen
dc.rights.accessRightsembargoedAccessen
dc.subject.keywordsCeramic-matrix composites (CMCs)en
dc.subject.keywordsHigh-temperature propertiesen
dc.subject.keywordsElectron microscopyen
dc.subject.keywordsJoints/joiningen
dc.identifier.essn1879-1069en
dc.journal.titleComposites Part B: Engineeringen
dc.page.final278en
dc.page.initial270en
dc.volume.number111en


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