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dc.creatorThompson, R.C.en
dc.creatorPak, T.T.en
dc.date.accessioned2015-09-04T16:05:09Zen
dc.date.available2015-09-04T16:05:09Zen
dc.date.issued2004-07en
dc.identifierPR_330en
dc.identifier.citationR.C. Thompson and T.T. Pak, “Advanced flywheel technology for space applications,” Proceedings, 37th Intersociety Energy Conversion Engineering Conference (IECEC 2002), Washington, D.C., U.S.A., July 29-31, 2002, pp. 153-156.en
dc.identifier.urihttp://hdl.handle.net/2152/30647en
dc.description.abstractFor spacecraft applications, energy storage sources are required to produce a high yield with minimum size and mass. Flywheel systems have the potential to fill this need while also providing attitude control for the guidance of the craft. Other advantages include on-board peak power management, extended service life (as compared to chemical batteries), and provisions for redundant systems with minimum effect on the projected payload of the craft. This paper reviews the results of flywheel design projects carried out at The University of Texas at Austin Center for Electromechanics (UT-CEM), discusses the role of composites in design development, and presents a detailed discussion of a flywheel design currently under study.en
dc.language.isoenen
dc.publisherIEEEen
dc.relation.ispartofCEM Publicationsen
dc.subjectRotating Machine Electrical Mechanical Systemsen
dc.subjectenergy storageen
dc.subjectflywheelen
dc.subjectsystemsen
dc.titleAdvanced Flywheel Technology for Space Applicationsen
dc.typeconference paperen
dc.description.departmentCenter for Electromechanicsen
dc.rights.restrictionopenen


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