Show simple item record

dc.contributor.authorTriantou, K.
dc.contributor.authorPerez, B.
dc.contributor.authorMarinou, A.
dc.contributor.authorFlorez, S.
dc.contributor.authorMergia, K.
dc.contributor.authorVekinis, G.
dc.contributor.authorBarcena, J.
dc.contributor.authorRotärmel, W.
dc.contributor.authorZuber, C.
dc.contributor.authorde Montbrun, À.
dc.date.accessioned2016-11-15T15:48:03Z
dc.date.available2016-11-15T15:48:03Z
dc.date.issued2017-01-01
dc.identifier.citationK. Triantou, B. Perez, A. Marinou, S. Florez, K. Mergia, G. Vekinis, J. Barcena, W. Rotärmel, C. Zuber, À. de Montbrun, Performance of cork and ceramic matrix composite joints for re-entry thermal protection structures, Composites Part B: Engineering, Volume 108, 1 January 2017, Pages 270-278, ISSN 1359-8368, http://dx.doi.org/10.1016/j.compositesb.2016.09.104.en
dc.identifier.issn1359-8368en
dc.identifier.urihttp://hdl.handle.net/11556/333
dc.description.abstractIn view of spacecraft re-entry applications into planetary atmospheres, hybrid thermal protection systems based on cork and ceramic matrix composites are investigated. Joints of NORCOAT LIÈGE cork with C/Csingle bondSiC ceramic matrix composite were fabricated using a) high temperature commercial inorganic adhesives and b) in-situ polymerization of the cork on top of the CMC. Mechanical shear tests under ambient conditions and in liquid nitrogen are carried out. The ultimate shear strength of all the adhesive joints at room temperature varies between 0.52 and 0.78 MPa and is similar to that of the in-situ joints. At liquid nitrogen temperature the shear strength is enhanced by up to 80%, but the ultimate shear strain decreases up to 55%. The failure mode is discussed for the two types of the fabrication procedure.en
dc.description.sponsorshipFP7 framework, European Project ‘‘HYDRA’’ (G.A. n. 283797), European Commission.en
dc.language.isoengen
dc.publisherELSEVIER SCI LTD, THE BOULEVARD, LANGFORD LANE, KIDLINGTON, OXFORD OX5 1GB, OXON, ENGLANDen
dc.titlePerformance of cork and ceramic matrix composite joints for re-entry thermal protection structuresen
dc.typearticleen
dc.identifier.doi10.1016/j.compositesb.2016.09.104en
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.keywordsCork based compositesen
dc.subject.keywordsCeramic matrix composites (CMCs)en
dc.subject.keywordsJoints/joiningen
dc.subject.keywordsThermo-mechanicalen
dc.subject.keywordsAerospaceen
dc.journal.titleComposites Part B: Engineeringen
dc.page.final278en
dc.page.initial270en
dc.volume.number108en


Files in this item

Thumbnail

    Show simple item record