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dc.contributorBogin, Gregory E.
dc.contributorSaldana, Mario H.
dc.contributor.authorSardin, Juliette
dc.date2013-08
dc.date.accessioned2007-01-03T06:05:57Z
dc.date.accessioned2022-02-03T10:23:43Z
dc.date.available2007-01-03T06:05:57Z
dc.date.available2022-02-03T10:23:43Z
dc.identifier.urihttps://hdl.handle.net/11124/322
dc.identifier.urihttp://dx.doi.org/10.25676/11124/322
dc.description.abstractThe Air Force's scramjet (supersonic combustion ramjet) is a jet engine in which combustion takes place in supersonic airflow. As scramjet flight speeds increase to supersonic and hypersonic regimes, the temperature of the ram air taken on board the vehicle becomes too high to cool the structure. Therefore, it is necessary to use a fuel that undergoes endothermic cracking as the primary coolant. The primary focus of this project is to develop a fundamental understanding of the coupled homogeneous and heterogeneous reactions that occur during endothermic fuel cracking; which will be partly accomplished through the investigation of gas-phase and surface reaction interactions in a high pressure flow reactor.
dc.description.sponsorshipAir Force Office of Scientific Research, Grant No. FA9550-12-1-0495.
dc.format.mediumposters
dc.languageEnglish
dc.language.isoeng
dc.publisherColorado School of Mines. Arthur Lakes Library
dc.relation.ispartof2013 NSF Research Experiences for Undergraduates posters and presentations
dc.rightsCopyright of the original work is retained by the author.
dc.subjectREMRSEC
dc.titleExperimental investigation of endothermic fuel cracking for cooling hypersonic vehicles
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