dc.contributor.author | Triantou, K. | |
dc.contributor.author | Mergia, K. | |
dc.contributor.author | Marinou, A. | |
dc.contributor.author | Vekinis, G. | |
dc.contributor.author | Bárcena, Jorge | |
dc.contributor.author | Florez, S. | |
dc.contributor.author | Perez, B. | |
dc.contributor.author | Pinaud, G. | |
dc.contributor.author | Bouilly, J.M. | |
dc.contributor.author | Fischer, W.P.P. | |
dc.date.accessioned | 2016-06-21T06:44:20Z | |
dc.date.available | 2016-06-21T06:44:20Z | |
dc.date.issued | 2015-04 | |
dc.identifier.citation | JOURNAL OF MATERIALS ENGINEERING AND PERFORMANCE, vol.24, issue 4 (2015), pp.1452-1461 | en |
dc.identifier.issn | 1059-9495 | en |
dc.identifier.uri | http://hdl.handle.net/11556/257 | |
dc.description.abstract | In view of spacecraft re-entry applications into planetary atmospheres, hybrid thermal protection systems based on layered composites of ablative materials and ceramic matrix composites are investigated. Joints of ASTERM (TM) lightweight ablative material with C-f/SiC (SICARBON (TM)) were fabricated using commercial high temperature inorganic adhesives. Sound joints without defects are produced and very good bonding of the adhesive with both base materials is observed. Mechanical shear tests under ambient conditions and in liquid nitrogen show that mechanical failure always takes place inside the ablative material with no decohesion of the interface of the adhesive layer with the bonded materials. Surface treatment of the ablative surface prior to bonding enhances both the shear strength and the ultimate shear strain by up to about 60% | en |
dc.description.sponsorship | European Project "HYDRA" | en |
dc.language.iso | eng | en |
dc.publisher | SPRINGER, 233 SPRING ST, NEW YORK, NY 10013 USA | en |
dc.title | Novel Hybrid Ablative/Ceramic Layered Composite for Earth Re-entry Thermal Protection: Microstructural and Mechanical Performance | en |
dc.type | journal article | en |
dc.identifier.doi | 10.1007/s11665-015-1410-8 | en |
dc.isi | Yes | en |
dc.relation.projectID | info:eu-repo/grantAgreement/EC/FP7/283797/EU/HYBRID ABLATIVE DEVELOPMENT FOR RE-ENTRY IN PLANETARY ATMOSPHERIC THERMAL PROTECTION/HYDRA | en |
dc.rights.accessRights | embargoed access | en |
dc.subject.keywords | adhesives | en |
dc.subject.keywords | aerospace | en |
dc.subject.keywords | ceramic | en |
dc.subject.keywords | composites | en |
dc.subject.keywords | mechanical | en |
dc.subject.keywords | mycroscopy | en |
dc.subject.keywords | optical metallography | en |
dc.subject.keywords | static | en |
dc.subject.keywords | x-ray | en |