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Maximum propellant utilization in an electron-bombardment thrusterMaximum propellant utilization in electron bombardment ion thrusters using mercury for propellant
Document ID
19710026637
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kaufman, H. R. (NASA Lewis Research Center Cleveland, OH, United States)
Cohen, A. J. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1971
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-67921
E-6554
Report Number: NASA-TM-X-67921
Report Number: E-6554
Accession Number
71N36113
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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