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Life test of a xenon hollow cathode for a space plasma contractorA plasma contacting device using a hollow cathode for plasma production has been baselined for use on the Space Station. This application will require reliable, continuous operation of the cathode at electron emission currents of between 0.75 and 10 A for two years (17,500 hours). In order to validate life-time capability, a hollow cathode, operated in a diode configuration, has been tested for more than 8600 hours of stable discharge operation as of March 30, 1994. This cathode is operated at a steady-state emission current of 12.0 and a fixed xenon flow rate of 4.5 sccm. Discharge voltage and cathode temperature have remained relatively stable at approximately 12.9 V and 1260 C during the test. The test has experienced 7 shutdowns to date. In all instances, the cathode was reignited at about 42 V and resumed stable operation. This test represents the longest demonstration of stable operation of high current (greater than 1A) xenon hollow cathodes reported to date.
Document ID
19950027505
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sarver-Verhey, Timothy R.
(NYMA, 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
NAS 1.26:195403
NASA-CR-195403
E-9247
Meeting Information
Meeting: 1994 Tri-Serivce/NASA Cathode Workshop
Location: Cleveland, Oh
Country: United States
Start Date: March 29, 1994
End Date: March 31, 1994
Accession Number
95N33926
Funding Number(s)
PROJECT: RTOP 478-43-00
CONTRACT_GRANT: NAS3-27186
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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