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Description of a 2.3 kW power transformer for space applicationsThe principle features and special testing of a high voltage high power transformer designed and developed for space application are described. The transformer is operated in a series resonant inverter supplying beam power to a 30 cm mercury ion thruster. Electrical requirements include operation of 2.3 kW continuous power output, primary currents to 35 amps rms, and frequencies up to 20 kHz. High efficiency was obtained through detailed considerations of the tradeoffs available in core materials, wire selection, coil configurations and thermal control. A number of novel heat removal techniques are discussed which control the winding temperature using only the available conductive cooling.
Document ID
19790015177
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Hansen, I.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1979
Subject Category
Electronics And Electrical Engineering
Report/Patent Number
NASA-TM-79138
E-9976
Report Number: NASA-TM-79138
Report Number: E-9976
Meeting Information
Meeting: Aerospace High Voltage Workshop
Location: Anaheim, CA
Country: United States
Start Date: February 26, 1979
End Date: February 27, 1979
Sponsors: IEEE, Intern. Electron. Packaging Soc., Aerospace Electron. Systems Soc.
Accession Number
79N23348
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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