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High Efficiency Synchronous Rectification in Spacecraft

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dc.contributor.author Krauhamer, S. en_US
dc.contributor.author Das, R. en_US
dc.contributor.author Vorperian, V. en_US
dc.contributor.author White, J. en_US
dc.contributor.author Bennett, J. en_US
dc.contributor.author Rogers, D. en_US
dc.date.accessioned 2004-10-06T02:34:32Z
dc.date.available 2004-10-06T02:34:32Z
dc.date.issued 1993-08-23 en_US
dc.identifier.citation Graz, Austria en_US
dc.identifier.clearanceno 93-0863 en_US
dc.identifier.uri http://hdl.handle.net/2014/35282
dc.description.abstract This paper examines the implementaion of MOSFETs as synchronous rectifiers which results in a substantial improvement in power processing efficency and therefore may result in significant reduction of spacecraft mass and volum for the same payload. en_US
dc.format.extent 535892 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other Spacecraft Power en_US
dc.title High Efficiency Synchronous Rectification in Spacecraft en_US


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