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Neutralizer Characterization of a NEXT Multi-Thruster Array With Electrostatic ProbesNeutralizers in a multi-thruster array configuration were characterized using conventional diagnostics such as peak-to-peak keeper oscillation amplitude as well as unconventional methods which featured the application of electrostatic probes. The response of the array local plasma environment to neutralizer flow rate changes were documented using Langmuir probes and retarding potential analyzers. Such characterization is necessary for system efficiency and stability optimization. Because the local plasma environment was measured in conjunction with the neutralizer characterization, particle fluxes at the array and thus array lifetime impacts associated with neutralizer operating mode could also be investigated. Neutralizer operating condition was documented for a number of multithruster array configurations ranging from three-engines, three-neutralizers to a single engine, one-neutralizer all as a function of neutralizer flow rate.
Document ID
20060028461
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Foster, John E.
(NASA Glenn Research Center Cleveland, OH, United States)
Patterson, Michael
(NASA Glenn Research Center Cleveland, OH, United States)
Pencil, Eric
(NASA Glenn Research Center Cleveland, OH, United States)
McEwen, Heather
(NASA Glenn Research Center Cleveland, OH, United States)
Diaz, Esther
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
July 1, 2006
Subject Category
Electronics And Electrical Engineering
Report/Patent Number
NASA/TM-2006-214403
E-15682
Report Number: NASA/TM-2006-214403
Report Number: E-15682
Meeting Information
Meeting: 42nd Joint Propulsion Conference and Exhibit
Location: Sacramento, CA
Country: United States
Start Date: July 9, 2006
End Date: July 12, 2006
Sponsors: Society of Automotive Engineers, Inc., American Inst. of Aeronautics and Astronautics, American Society for Engineering Education, American Society of Mechanical Engineers
Funding Number(s)
WBS: WBS 22-973-80-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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