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Experimental Investigation from the Operation of a 2 kW Brayton Power Conversion Unit and a Xenon Ion ThrusterA 2kW Brayton Power Conversion Unit (PCU) and a xenon ion thruster were integrated with a Power Management and Distribution (PMAD) system as part of a Nuclear Electric Propulsion (NEP) Testbed at NASA's Glenn Research Center. Brayton Converters and ion thrusters are potential candidates for use on future high power NEP mission such as the proposed Jupiter Icy Moons Orbiter (JIMO). The use of a existing lower power test hardware provided a cost effective means to investigate the critical electrical interface between the power conversion system and the propulsion system. The testing successfully demonstrated compatible electrical operations between the converter and the thruster, including end-to-end electric power throughput, high efficiency AC to DC conversion, and thruster recycle fault protection. The details of this demonstration are reported herein.
Document ID
20040111431
Document Type
Conference Paper
Authors
Hervol, David
(Analex Corp. Cleveland, OH, United States)
Mason, Lee
(NASA Glenn Research Center Cleveland, OH, United States)
Birchenough, Art
(NASA Glenn Research Center Cleveland, OH, United States)
Pinero, Luis
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 21, 2013
Publication Date
January 1, 2004
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Space Technology and Applications International Forum(Albuquerque, NM)
Funding Number(s)
CONTRACT_GRANT: NAS3-00145
WBS: WBS 22-973-80-10
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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