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A survey of Kaufman thruster cathodes.A survey is presented of various cathodes which have been developed and used in the Kaufman ion thruster. The electron-bombardment type ion source used in the thruster 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 describing 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 and should offer further performance and life improvements.
Document ID
19720030767
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Weigand, A. J.
Nakanishi, S.
(NASA Lewis Research Center Cleveland, Ohio, United States)
Date Acquired
August 6, 2013
Publication Date
October 1, 1971
Subject Category
Propulsion Systems
Meeting Information
Meeting: American Physical Society and Brookhaven National Laboratory, Symposium on Ion Sources and Formation of Ion Beams
Location: Upton, NY
Start Date: October 19, 1971
End Date: October 21, 1971
Sponsors: Brookhaven National Laboratory, American Physical Society
Accession Number
72A14433
Distribution Limits
Public
Copyright
Other

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