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Hg ion thruster component testingElectron bombardment thrusters, under development to provide both auxiliary and primary propulsion functions for a large variety of space missions are tested. Thruster design verification which requires life tests of durations of the order of the time anticipated in space applications, are discussed. The life time and reliability of an electron bombardment thruster is dependent upon the performance of several critical components including cathodes, vaporizers, and isolators. The performances of the cathode, vaporizer, and propellant isolaters during fatigue analyses are examined.
Document ID
19800004904
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mantenieks, M. A.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1979
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-TM-79287
E-230
Report Number: NASA-TM-79287
Report Number: E-230
Meeting Information
Meeting: Intern. Conf. on Elec. Propulsion
Location: Princeton, N. J.
Country: United States
Start Date: October 30, 1979
End Date: November 1, 1979
Sponsors: AIAA, DGLR
Accession Number
80N13159
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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