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Multi-Kilowatt Power Module for High-Power Hall ThrustersFuture NASA missions will require high-performance electric propulsion systems. Hall thrusters are being developed at NASA Glenn for high-power, high-specific impulse operation. These thrusters operate at power levels up to 50 kW of power and discharge voltages in excess of 600 V. A parallel effort is being conducted to develop power electronics for these thrusters that push the technology beyond the 5kW state-of-the-art power level. A 10 kW power module was designed to produce an output of 500 V and 20 A from a nominal 100 V input. Resistive load tests revealed efficiencies in excess of 96 percent. Load current share and phase synchronization circuits were designed and tested that will allow connecting multiple modules in parallel to process higher power.
Document ID
20050161945
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Pinero, Luis R.
(NASA Glenn Research Center Cleveland, OH, United States)
Bowers, Glen E.
(Akima Corp. Fairview Park, OH, United States)
Date Acquired
September 7, 2013
Publication Date
March 1, 2005
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA Paper 2004-3973
NASA/TM-2005-213348
E-14816
Report Number: AIAA Paper 2004-3973
Report Number: NASA/TM-2005-213348
Report Number: E-14816
Meeting Information
Meeting: 40th Joint Propulsion Conference and Exhibit
Location: Fort Lauderdale, FL
Country: United States
Start Date: July 11, 2004
End Date: July 14, 2004
Sponsors: American Society for Electrical Engineers, Society of Automotive Engineers, Inc., American Society of Mechanical Engineers, American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 22-319-20-F2
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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