Publication:
Synergistic effect of nano-additives and tackifier resins on hybrid rocket fuel performance

dc.contributor.coauthorBaysal, Mustafa
dc.contributor.coauthorBilge, Kaan
dc.contributor.coauthorKokal, Uğur
dc.contributor.departmentDepartment of Mechanical Engineering
dc.contributor.departmentN/A
dc.contributor.departmentN/A
dc.contributor.kuauthorEmerce, Nur Ber
dc.contributor.kuauthorKarabeyoğlu, Mustafa Arif
dc.contributor.kuauthorYıldız, Utku Can
dc.contributor.kuprofileFaculty Member
dc.contributor.kuprofilePhD Student
dc.contributor.kuprofileMaster Student
dc.contributor.otherDepartment of Mechanical Engineering
dc.contributor.schoolcollegeinstituteCollege of Engineering
dc.contributor.schoolcollegeinstituteGraduate School of Sciences and Engineering
dc.contributor.schoolcollegeinstituteGraduate School of Sciences and Engineering
dc.contributor.yokid114595
dc.contributor.yokidN/A
dc.contributor.yokidN/A
dc.date.accessioned2024-11-09T22:56:09Z
dc.date.issued2020
dc.description.abstractConventional paraffin based hybrid rocket fuels have inherently weak mechanical performance. This paper aims to investigate potential mechanical toughening achieved by the co-addition of tackifier resins and different particles as additives to increase the mechanical performance without effecting the fuel flow characteristics. A styrenated terpene tackifier resin and 4 different particles are considered as additives to considered base fuel formulations(BF) (containing dominantly macro-crystalline wax). Integrated particles are classified as i) nano-silica powder (spherical) ii) carbon black (spherical) iii) activated carbon (random shape, high surface area) and iv) multi-walled carbon nanotubes (tubular, high aspect ratio). An initial screening effort is performed to fuel blends with 0.1 wt.% particle concentration and 10 wt.% tackifier resin. Mode I fracture toughness and work of fracture of the obtained fuel samples are measured by notched four point bending tests. Parallelly, melt viscosity of the samples are recorded in order to approximate the fuel regression rate. Particle/fuel interactions are portrayed by differential calorimetry (DSC) analysis. Particle type screening efforts suggested that MWCNTs are best suitable candidates due to their ”pin” like structure that provides higher deformability and fracture toughness to fuel formulations. Then a weight fraction screening is performed to to fuel blends with three different MWCNT concentrations (0.01, 0.1 and 0.25 wt.%) in order to identify the optimum amount of MWCNT to be considered. Results suggested that when used at very low amounts 0.01 wt.%, the effectiveness and processability of MWCNTs increases. Furthermore, when co-added with tackifier resins, a synergistic ”adhere” and ”pin” toughening strategy can be obtained that significantly increases the fracture toughness of fuel blends with no increase in melt viscosity. Being cost effective, easy to process and superior such formulations are found to increase the resistance of hybrid rocket fuel grains against mechanical failures during operation.
dc.description.indexedbyScopus
dc.description.openaccessYES
dc.description.publisherscopeInternational
dc.description.volume2020
dc.identifier.doi10.2514/6.2020-3738
dc.identifier.isbn978-162410602-6
dc.identifier.linkhttps://www.scopus.com/inward/record.uri?eid=2-s2.0-85091290061&doi=10.2514%2f6.2020-3738&partnerID=40&md5=0ea8a0dc156a7271ea26e8cc0db60bd5
dc.identifier.scopus2-s2.0-85091290061
dc.identifier.urihttps://dx.doi.org/10.2514/6.2020-3738
dc.identifier.urihttps://hdl.handle.net/20.500.14288/7329
dc.keywordsAspect ratio
dc.keywordsBending tests
dc.keywordsCarbon black
dc.keywordsCost effectiveness
dc.keywordsFailure (mechanical)
dc.keywordsFracture toughness
dc.keywordsMultiwalled carbon nanotubes (MWCN)
dc.keywordsPropulsion
dc.keywordsResins
dc.keywordsRockets
dc.keywordsSilica
dc.keywordsViscosity
dc.keywordsDifferential calorimetry
dc.keywordsFour-point bending test
dc.keywordsFuel regression rates
dc.keywordsFuel-flow characteristics
dc.keywordsMechanical failures
dc.keywordsMechanical performance
dc.keywordsMode-i fracture toughness
dc.keywordsParticle concentrations
dc.keywordsFuel additives
dc.languageEnglish
dc.publisherAmerican Institute of Aeronautics and Astronautics
dc.sourceAIAA Propulsion and Energy 2020 Forum
dc.subjectEngineering
dc.titleSynergistic effect of nano-additives and tackifier resins on hybrid rocket fuel performance
dc.typeConference proceeding
dspace.entity.typePublication
local.contributor.authorid0000-0002-5071-6133
local.contributor.authorid0000-0002-0927-6586
local.contributor.authoridN/A
local.contributor.kuauthorKarabeyoğlu, Mustafa Arif
local.contributor.kuauthorEmerce, Nur Ber
local.contributor.kuauthorYıldız, Utku Can
relation.isOrgUnitOfPublicationba2836f3-206d-4724-918c-f598f0086a36
relation.isOrgUnitOfPublication.latestForDiscoveryba2836f3-206d-4724-918c-f598f0086a36

Files