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dc.contributor.authorMurray, Brendan R.
dc.contributor.authorDoyle, Adrian
dc.contributor.authorFeerick, P. J.
dc.contributor.authorSemprimoschnig, Christopher O.A.
dc.contributor.authorLeen, Sean B.
dc.contributor.authorÓ Brádaigh, Conchúr M.
dc.date.accessioned2019-12-02T15:15:15Z
dc.date.available2019-12-02T15:15:15Z
dc.date.issued2017-07-15
dc.identifier.citationMurray, Brendan R., Doyle, Adrian, Feerick, P. J., Semprimoschnig, Christopher O. A., Leen, Sean B., & Ó Brádaigh, Conchúr M. (2017). Rotational moulding of PEEK polymer liners with carbon fibre/PEEK over tape-placement for space cryogenic fuel tanks. Materials & Design, 132, 567-581. doi: https://doi.org/10.1016/j.matdes.2017.07.026en_IE
dc.identifier.issn0264-1275
dc.identifier.urihttp://hdl.handle.net/10379/15604
dc.description.abstractPEEK polymers are investigated as replacement materials for metallic liners in composite overwrapped pressure vessels (COPVs) for fuel tank applications in space. A novel, integrally heated, rotational moulding tool has been developed to produce PEEK polymer liners, samples of which have then been overwrapped using CF/PEEK in a laser assisted tape-placement (LATP) process to produce demonstrator samples of a polymer lined COPV. Helium permeability testing has shown that the designs are capable of resisting leakage to acceptable levels for fuel storage, while X-ray CT scanning and cryogenic cycling have shown that the current design is capable of resisting crack growth over multiple cycles. Nano-indentation testing has shown that the LATP process has created a region of reduced modulus in the PEEK polymer at the surface of the liner where the CF/PEEK has been tape-laid. This laser-affected zone of reduced polymer modulus in the composite interface region has enabled an enhanced resistance to crack growth formations from thermal residual stresses in comparison to hot plate moulded test samples. (C) 2017 Elsevier Ltd. All rights reserved.en_IE
dc.description.sponsorshipThe authors would like to thank the Irish Research Council (IRC) (EPSPG/2011/66) and the European Space Agency (ESA) (B00015002) for joint funding of this research under the Network Partnering Initiative (NPI) and Innovation Triangle Initiative (ITI). They would also like to acknowledge the specific help and technical support provided by Michael Flanagan of NUI Galway, Derrick Doyle and Fintan Doyle of ÉireComposites Teo, and Dr. Terry McGrail and David Jones of the Irish Centre for Composites Research (ICOMP). A final thanks to Prof. Peter McHugh and Dr. Reyhaneh Neghabat Shirazi of NUI Galway for use and training with the nano-indentation testing equipment.en_IE
dc.formatapplication/pdfen_IE
dc.language.isoenen_IE
dc.publisherElsevieren_IE
dc.relation.ispartofMaterials & Designen
dc.rightsAttribution-NonCommercial-NoDerivs 3.0 Ireland
dc.rights.urihttps://creativecommons.org/licenses/by-nc-nd/3.0/ie/
dc.subjectPolymersen_IE
dc.subjectCompositesen_IE
dc.subjectLinersen_IE
dc.subjectCOPVsen_IE
dc.subjectCryogenic fuel tanksen_IE
dc.subjectPEEKen_IE
dc.subjectMECHANICAL-PROPERTIESen_IE
dc.subjectELASTIC-MODULUSen_IE
dc.subjectNONISOTHERMAL CRYSTALLIZATIONen_IE
dc.subjectGAS-PERMEABILITYen_IE
dc.subjectDAMAGEen_IE
dc.subjectNANOINDENTATIONen_IE
dc.subjectCOMPOSITESen_IE
dc.subjectCRYSTALLINITYen_IE
dc.subjectPERMEATIONen_IE
dc.subjectMODELen_IE
dc.titleRotational moulding of PEEK polymer liners with carbon fibre/PEEK over tape-placement for space cryogenic fuel tanksen_IE
dc.typeArticleen_IE
dc.date.updated2019-11-26T17:58:14Z
dc.identifier.doi10.1016/j.matdes.2017.07.026
dc.local.publishedsourcehttps://doi.org/10.1016/j.matdes.2017.07.026en_IE
dc.description.peer-reviewedpeer-reviewed
dc.contributor.funderIrish Research Councilen_IE
dc.contributor.funderEuropean Space Agencyen_IE
dc.internal.rssid13154912
dc.local.contactSean Leen, Mechanical & Biomedical Eng, Eng-2051, New Engineering Building, Nui Galway. 5955 Email: sean.leen@nuigalway.ie
dc.local.copyrightcheckedYes
dc.local.versionACCEPTED
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