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Extended test of a xenon hollow cathode for a space plasma contactorImplementation of a hollow cathode plasma contactor for charge control on the Space Station has required validation of long-life hollow cathodes. A test series of hollow cathodes and hollow cathode plasma contactors was initiated as part of the plasma contactor development program. An on-going wear-test of a hollow cathode has demonstrated cathode operation in excess of 4700 hours with small changes in operating parameters. The discharge experienced 4 shutdowns during the test, all of which were due to test facility failures or expellant replenishment. In all cases, the cathode was reignited at approximately 42 volts and resumed typical operation. This test represents the longest demonstrated stable operation of a high current (greater than 1A) xenon hollow cathode reported to date.
Document ID
19950010850
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sarver-Verhey, Timothy R.
(Sverdrup Technology, Inc. Brook Park, OH, United States)
Date Acquired
September 6, 2013
Publication Date
November 1, 1994
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
E-9246
NAS 1.26:195402
NASA-CR-195402
Report Number: E-9246
Report Number: NAS 1.26:195402
Report Number: NASA-CR-195402
Meeting Information
Meeting: International Electric Propulsion Conference
Location: Seattle, WA
Country: United States
Start Date: September 13, 1993
End Date: September 17, 1993
Accession Number
95N17265
Funding Number(s)
CONTRACT_GRANT: NAS3-25266
PROJECT: RTOP 506-42-31
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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