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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.departmentGraduate School of Sciences and Engineering
dc.contributor.kuauthorKara, Ozan
dc.contributor.programMechanical Engineering
dc.contributor.schoolcollegeinstituteGRADUATE SCHOOL OF SCIENCES AND ENGINEERING
dc.coverage.spatialİstanbul
dc.date.accessioned2024-11-09T21:50:34Z
dc.date.issued2021
dc.format.extentxix, 120 leaves. : tables ; 30 cm.
dc.identifier.urihttps://hdl.handle.net/20.500.14288/4163
dc.language.isoeng
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.titleIgnition capability of CO2 in hybrid rockets for mars ascent vehicles
dc.typeDissertation
dspace.entity.typePublication
local.contributor.kuauthorKara, Ozan
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