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Electron Backstreaming Mitigation via a Magnetic GridElectron backstreaming due to accelerator grid hole enlargement has been identified as a failure mechanism that will limit ion thruster service lifetime. Over extended periods of time as accelerator grid apertures enlarge due to erosion, ion thrusters are required to operate at increasingly higher accelerator grid voltages in order to prevent electron backstreaming. These higher voltages give rise to higher grid erosion rates, which in turn accelerates aperture enlargement. Presented here is an approach to mitigate the backflow of electrons into the engine by using a transverse magnetic field.
Document ID
20020038544
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Foster, John F.
(NASA Glenn Research Center Cleveland, OH United States)
Roman, Robert F.
(NASA Glenn Research Center Cleveland, OH United States)
Soulas, George C.
(NASA Glenn Research Center Cleveland, OH United States)
Patterson, Michael J.
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2002
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NAS 1.15:211283
NASA/TM-2002-211283
E-13083
IEPC-01-91
Report Number: NAS 1.15:211283
Report Number: NASA/TM-2002-211283
Report Number: E-13083
Report Number: IEPC-01-91
Meeting Information
Meeting: 27th International Electric Propulsion Conference
Location: Pasadena, CA
Country: United States
Start Date: October 14, 2001
End Date: October 19, 2001
Sponsors: NASA Headquarters, NASA Glenn Research Center, Jet Propulsion Lab., California Inst. of Tech., NASA Marshall Space Flight Center, Electric Rocket Propulsion Society, Air Force Research Lab., Centre National d'Etudes Spatiales
Funding Number(s)
PROJECT: RTOP 755-B4-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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