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A 20000-hour endurance test of a structurally and thermally integrated 5-cm diameter ion thruster main cathodeA 5-cm diameter mercury ion thruster main cathode has completed over 20,000 hours of operation in an ongoing lifetime endurance test. The cathode operating parameters remained at acceptable performance levels throughout the test, the first 9175 hours of which were part of a thruster endurance test. After 20,000 hours, the cathode discharge was easily restarted, the tip orifice indicated negligible erosion and the tip heater showed no degradation. The cathode-isolator- vaporizer assembly, a major thruster subsystem, has thus successfully demonstrated an operational lifetime capability of 20,000 hours, which is the lifetime goal of the 8-cm diameter auxiliary propulsion ion thruster.
Document ID
19750008547
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Wintucky, E. G.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1975
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-TM-X-71660
Meeting Information
Meeting: 11th AIAA Elec. Propulsion Conf
Location: New Orleans, LA
Country: United States
Start Date: March 19, 1975
End Date: March 21, 1975
Accession Number
75N16619
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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