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A 13000-hour test of a mercury hollow cathodeA mercury-fed hollow cathode was tested for 12,979 hours in a bell jar at SERT 2 neutralizer operating conditions. The net electron current drawn to a collector was 0.25 ampere at average collector voltages between 21.8 and 36.7 volts. The mercury flow rate was varied from 5.6 to 30.8 equivalent milliamperes to give stable operation at the desired electrode voltages and currents. Variations with time in the neutralizer discharge characteristics were observed and hypothesized to be related to changes in the cathode orifice dimensions and the availability of electron emissive material. A facility failure caused abnormal test conditions for the last 876 hours and led to the cathode heater failure which concluded the test.
Document ID
19730016066
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Rawlin, V. K.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1973
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-2785
E-7163
Report Number: NASA-TM-X-2785
Report Number: E-7163
Accession Number
73N24793
Funding Number(s)
PROJECT: RTOP 758-57
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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