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Uncertainty Quantification of Modeled Electron Backstreaming Failure for the NEXT Ion ThrusterExcessive electron back streaming is one of the primary life-limiting failure modes for gridded ion thrusters. Physics-based modeling of the optics grid erosion and electron back streaming margins is augmented with statistical uncertainty quantification techniques to generate a life expectancy distribution of this particular failure mechanism for the NEXT ion thruster. Generation of distributions instead of a single point estimate provide a more comprehensive picture of thruster failure probabilities and life expectation for various mission applications.







Document ID
20190032079
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Yim, John T.
(NASA Glenn Research Center Cleveland, OH, United States)
Williams, George J., Jr.
(NASA Glenn Research Center Cleveland, OH, United States)
Shastry, Rohit
(NASA Glenn Research Center Cleveland, OH, United States)
Soulas, George C.
(NASA Glenn Research Center Cleveland, OH, United States)
Chaplin, Vernon H.
(Jet Propulsion Laboratory (JPL), California Institute of Technology (CalTech) Pasadena, CA, United States)
Polk, James E.
(Jet Propulsion Laboratory (JPL), California Institute of Technology (CalTech) Pasadena, CA, United States)
Date Acquired
October 15, 2019
Publication Date
September 15, 2019
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
GRC-E-DAA-TN72417
IEPC-2019-722
Report Number: GRC-E-DAA-TN72417
Report Number: IEPC-2019-722
Meeting Information
Meeting: International Electric Propulsion Conference
Location: Vienna
Country: Austria
Start Date: September 15, 2019
End Date: September 20, 2019
Sponsors: Bundesministerium fuer Verkehr
Funding Number(s)
WBS: 336763.01.05.02.04.05.01
Distribution Limits
Public
Copyright
Public Use Permitted.
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