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A survey of Kaufman thruster cathodesA survey is presented of the various cathodes which were developed and used in the Kaufman ion thruster. The electron bombardment type ion source is briefly described. The general design, operating characteristics, and power requirements are shown for each type of cathode from the refractory metals used in 1960 to the plasma discharge hollow cathodes of today. A detailed discussion of the hollow cathode is given, including starting and cyclic operating characteristics as well as more fundamental design parameters. Tests to date show that the plasma hollow cathode is an efficient electron source with demonstrated durability over 10,000 hours.
Document ID
19720018956
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Weigand, A. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Nakanishi, S.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 6, 2013
Publication Date
October 1, 1971
Publication Information
Publication: BNL Proc. of the Symp. on Ion Sources and Formation of Ion Beams
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-68386
Accession Number
72N26606
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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