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High Performance Power Module for Hall Effect ThrustersPrevious efforts to develop power electronics for Hall thruster systems have targeted the 1 to 5 kW power range and an output voltage of approximately 300 V. New Hall thrusters are being developed for higher power, higher specific impulse, and multi-mode operation. These thrusters require up to 50 kW of power and a discharge voltage in excess of 600 V. Modular power supplies can process more power with higher efficiency at the expense of complexity. A 1 kW discharge power module was designed, built and integrated with a Hall thruster. The breadboard module has a power conversion efficiency in excess of 96 percent and weighs only 0.765 kg. This module will be used to develop a kW, multi-kW, and high voltage power processors.
Document ID
20030003703
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Pinero, Luis R.
(NASA Glenn Research Center Cleveland, OH United States)
Peterson, Peter Y.
(QSS Group, Inc. Cleveland, OH United States)
Bowers, Glen E.
(Akima Corp. Fairview Park, OH United States)
Date Acquired
September 7, 2013
Publication Date
September 1, 2002
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
E-13556
NAS 1.15:211874
NASA/TM-2002-211874
AIAA Paper 2002-3947
Report Number: E-13556
Report Number: NAS 1.15:211874
Report Number: NASA/TM-2002-211874
Report Number: AIAA Paper 2002-3947
Meeting Information
Meeting: 38th Joint Propulsion Conference and Exhibit
Location: Indianapolis, IN
Country: United States
Start Date: July 7, 2002
End Date: July 10, 2002
Sponsors: American Society of Mechanical Engineers, American Society for Electrical Engineers, Society of Automotive Engineers, Inc., American Inst. of Aeronautics and Astronautics
Funding Number(s)
PROJECT: RTOP 755-B4-05
Distribution Limits
Public
Copyright
Public Use Permitted.
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