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Effect of thrustor arcing on ion rocket system designElectrode arcing effects on ion rocket thrustor system design
Document ID
19640018167
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Stover, J. B. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
September 2, 1964
Subject Category
Propellants
Report/Patent Number
NASA-TM-X-52045
Report Number: NASA-TM-X-52045
Accession Number
64N28081
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
THRUSTOR
IONIC PROPULSION

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