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Investigation of Rectifier Diode Failures in the NEXT-C Power Processing UnitNASA's Evolutionary Xenon Thruster-Commercial (NEXT-C) project is tasked with developing flight electric propulsion systems, including both thrusters and power processing units (PPUs). In 2018, the beam supply in a NEXT-C engineering prototype PPU experienced an output rectifier diode failure during development thermal-vacuum testing. A failure investigation led by NASA GRC identified the root cause of the failure as a thermal runaway caused by increased reverse recovery losses in the diodes when the PPU was run at its maximum operating temperature. Significant reverse recovery performance variations were identified in diodes with the same part number but manufactured by different vendors. The failure investigation was able to collect evidence of the increased reverse recovery and replicate the diode failures in a controlled laboratory environment.
Document ID
20210018272
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
George L Thomas
(Glenn Research Center Cleveland, Ohio, United States)
Henry B Fain
(Glenn Research Center Cleveland, Ohio, United States)
David C Pike
(Glenn Research Center Cleveland, Ohio, United States)
Luis R Pinero
(Glenn Research Center Cleveland, Ohio, United States)
Marcelo C Gonzalez
(Glenn Research Center Cleveland, Ohio, United States)
Robert J Scheidegger
(Glenn Research Center Cleveland, Ohio, United States)
Scott R Panko
(HX5, LLC)
Arthur G Birchenough
(HX5, LLC)
Date Acquired
July 6, 2021
Subject Category
Aircraft Propulsion And Power
Meeting Information
Meeting: 2021 AIAA Propulsion and Energy Forum
Location: Virtual
Country: US
Start Date: August 9, 2021
End Date: August 11, 2021
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 265759.06.01.01
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
Single Expert
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