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Please use this identifier to cite or link to this item: https://hdl.handle.net/2440/18971
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dc.contributor.authorIde, Kym Martinen
dc.date.issued1997en
dc.identifier.urihttp://hdl.handle.net/2440/18971-
dc.descriptionBibliography: leaves 190-196.en
dc.descriptionvi, 197 leaves : ill. ; 30 cm.en
dc.description.abstractThis thesis analyses the way in which ageing, temperature and strain-rate affect the thermal and fracture properties of the polymeric components in the PICTOR rocket motor. The change in the thermal expansion behaviour of the propellant, inhibitor, epoxy and insulation is investigated.en
dc.format.extent136247 bytesen
dc.format.mimetypeapplication/pdfen
dc.language.isoenen
dc.subject.lcshThermal stresses.en
dc.subject.lcshRocket engines.en
dc.subject.lcshPolymeric composites Thermal properties.en
dc.subject.lcshFracture mechanics.en
dc.titleThermal and fracture behaviour of rocket motor materials / by Kim Martin Ide.en
dc.typeThesisen
dc.contributor.schoolDept. of Chemical Engineeringen
dc.provenanceThis electronic version is made publicly available by the University of Adelaide in accordance with its open access policy for student theses. Copyright in this thesis remains with the author. This thesis may incorporate third party material which has been used by the author pursuant to Fair Dealing exception. If you are the author of this thesis and do not wish it to be made publicly available or If you are the owner of any included third party copyright material you wish to be removed from this electronic version, please complete the take down form located at: http://www.adelaide.edu.au/legalsen
dc.description.dissertationThesis (Ph.D.)--University of Adelaide, Dept. of Chemical Engineering, 1997?en
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