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dc.creatorLeachman, Jacob
dc.creatorStreet, Melissa Jean
dc.creatorGraham, Teira
dc.date.accessioned2015-11-25T22:09:29Z
dc.date.available2015-11-25T22:09:29Z
dc.date.issued2012
dc.identifier.urihttp://hdl.handle.net/2376/5650
dc.description.abstractAs the use and applications of Unmanned Aerial Vehicles (UAV) expand, the need for a lighter weight fuel allowing for longer duration flights has become the primary limiting factor in the advancement of these vehicles. To extend the operational envelope of UAV, onboard condensed hydrogen storage for missions exceeding one week is necessary. Currently, large spherical liquid hydrogen tanks that are pressurized with external helium tanks or electronic heating elements are utilized for this purpose. However, the mass, size, and power consumption of the fuel storage tank and fuel pressurization system significantly limit the flight envelope of UAV. In an effort to alleviate these issues, this paper investigates the technological feasibility of orthohydrogen-parahydrogen catalysis as a method of fuel pressurization. Typical pressurization requirements for takeoff, cruise, and landing are reviewed. Calculations of the catalyst system mass and response time are presented.en_US
dc.languageEnglish
dc.publisherProceedings of the Cryogenic Engineering Conference–CEC: Advances in Cryogenic Engineeringen_US
dc.rightsCopyright 2012, American Institute of Physics. This article may be downloaded for personal use only. Any other use requires prior permission of the author and the American Institute of Physics. The following article appeared in Transactions of the Cryogenic Engineering Conference–CEC: Advances in Cryogenic Engineering. It may be found at http://scitation.aip.org/content/aip/proceeding/aipcp/1218
dc.rightsopenAccess
dc.rights.urihttp://rightsstatements.org/vocab/InC/1.0/
dc.rights.urihttp://purl.org/eprint/accessRights/OpenAccess
dc.subjectAdvanced vehiclesen_US
dc.subjectFuel cell vehiclesen_US
dc.subjectCatalysisen_US
dc.subjectHydrogen storageen_US
dc.titleCatalytic pressurization of liquid hydrogen fuel tanks for unmanned aerial vehicles
dc.typeText
dc.description.citationJ.W. Leachman, M. Street, and T. Graham, Catalytic pressurization of liquid hydrogen fuel tanks for Unmanned Aerial Vehicles, Advances in Cryogenic Engineering-Proceedings of the 2011 Cryogenic Engineering Conference-CEC, 57 (2012) 1261-1267.


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  • Leachman, Jacob
    This collection features research by Jacob Leachman, assistant professor of Mechanical and Materials Engineering (MME) at Washington State University.

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