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High Efficiency Synchronous Rectification in SpacecraftThis 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.
Document ID
20060038951
Acquisition Source
Jet Propulsion Laboratory
Document Type
Preprint (Draft being sent to journal)
External Source(s)
Authors
Krauhamer, S.
Das, R.
Vorperian, V.
White, J.
Bennett, J.
Rogers, D.
Date Acquired
August 23, 2013
Publication Date
August 23, 1993
Distribution Limits
Public
Copyright
Other
Keywords
Spacecraft Power

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