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Ignition capability of CO2 in hybrid rockets for mars ascent vehicles

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dc.contributor.advisorKarabeyoğlu, Mustafa Arif
dc.contributor.advisorid0000-0002-5071-6133
dc.contributor.authorKara, Ozan
dc.contributor.instituteKoç University Graduate School of Sciences and Engineering
dc.contributor.programMechanical Engineering
dc.contributor.yokid114595
dc.date.accessioned2024-11-09T21:50:34Z
dc.date.issued2021
dc.descriptionxix, 120 leaves. : tables ; 30 cm.
dc.identifier.urihttps://hdl.handle.net/20.500.14288/4163
dc.languageEnglish
dc.publisherKoç University
dc.relation.collectionKU Theses and Dissertations
dc.rightsrestrictedAccess
dc.rights.copyrightsnote© All Rights Reserved. Accessible to Koç University Affiliated Users Only!
dc.subjectCarbon dioxide
dc.subjectLiquid propellant rockets
dc.subjectRocket engines, Combustion
dc.subjectAeronautics
dc.subjectPower resources
dc.thesis.degreeDoctoral Degree
dc.thesis.grantorİstanbul
dc.titleIgnition capability of CO2 in hybrid rockets for mars ascent vehicles
dc.typeDissertation
dspace.entity.typePublication
relation.isAdvisorOfThesis13632a12-34b4-4e1d-9e16-08174b53daf9
relation.isAdvisorOfThesis.latestForDiscovery13632a12-34b4-4e1d-9e16-08174b53daf9

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