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Hall Current Plasma Source Having a Center-Mounted or a Surface-Mounted CathodeA miniature Hall current plasma source apparatus having magnetic shielding of the walls from ionized plasma, an integrated discharge channel and gas distributor, an instant-start hollow cathode mounted to the plasma source, and an externally mounted keeper, is described. The apparatus offers advantages over other Hall current plasma sources having similar power levels, including: lower mass, longer lifetime, lower part count including fewer power supplies, and the ability to be continuously adjustable to lower average power levels using pulsed operation and adjustment of the pulse duty cycle. The Hall current plasma source can provide propulsion for small spacecraft that either do not have sufficient power to accommodate a propulsion system or do not have available volume to incorporate the larger propulsion systems currently available. The present low-power Hall current plasma source can be used to provide energetic ions to assist the deposition of thin films in plasma processing applications.
Document ID
20180002676
Acquisition Source
Marshall Space Flight Center
Document Type
Other - Patent
Authors
Martinez, Rafael A.
Williams, John D.
Moritz, Jr., Joel A.
Farnell, Casey C.
Date Acquired
May 3, 2018
Publication Date
April 3, 2018
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
Patent Number: US-Patent-9,934,929
Patent Application Number: US-Patent-Appl-SN-15/424,385
Funding Number(s)
CONTRACT_GRANT: NNM15AA22P
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-9,934,929
Patent Application
US-Patent-Appl-SN-15/424,385
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