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Effect of neutralizer position on accelerator wear for a 30 centimeter diameter ion bombardment thrusterNeutralizer location for minimum accelerator erosion on 30 centimeter diameter ion bombardment thruster
Document ID
19710026638
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Bechtel, R. T. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
September 1, 1971
Subject Category
Propulsion Systems
Report/Patent Number
E-6574
NASA-TM-X-67926
Report Number: E-6574
Report Number: NASA-TM-X-67926
Accession Number
71N36114
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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