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Development of High-Power Hall Thruster Power Processing Units at NASA GRCNASA GRC successfully designed, built and tested four different power processor concepts for high power Hall thrusters. Each design satisfies unique goals including the evaluation of a novel silicon carbide semiconductor technology, validation of innovative circuits to overcome the problems with high input voltage converter design, development of a direct-drive unit to demonstrate potential benefits, or simply identification of lessonslearned from the development of a PPU using a conventional design approach. Any of these designs could be developed further to satisfy NASA's needs for high power electric propulsion in the near future.
Document ID
20150023095
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Pinero, Luis R.
(NASA Glenn Research Center Cleveland, OH United States)
Bozak, Karin E.
(NASA Glenn Research Center Cleveland, OH United States)
Santiago, Walter
(NASA Glenn Research Center Cleveland, OH United States)
Scheidegger, Robert J.
(NASA Glenn Research Center Cleveland, OH United States)
Birchenough, Arthur G.
(Vantage Partners, LLC Brook Park, OH, United States)
Date Acquired
December 15, 2015
Publication Date
July 27, 2015
Subject Category
Spacecraft Propulsion And Power
Electronics And Electrical Engineering
Report/Patent Number
GRC-E-DAA-TN24681
Meeting Information
Meeting: AIAA/SAE/ASEE Joint Propulsion Conference
Location: Orlando, FL
Country: United States
Start Date: July 27, 2015
End Date: July 29, 2015
Sponsors: American Inst. of Aeronautics and Astronautics, Society of Automotive Engineers, Inc., American Society for Engineering Education (ASEE)
Funding Number(s)
CONTRACT_GRANT: NNC12BA01B
WBS: WBS 729200.06.03.05
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Spacecraft Power Supplies
Hall Thruster
Electric Propulsion
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