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Maximum propellant utilization in an electron-bombardment thruster.Current theory and experimental data on propellant utilization in electron-bombardment ion thrusters are reviewed. Because the majority of investigations have been conducted with mercury, the presentation emphasizes that propellant. The results are presented in as general a form as possible to facilitate use in areas other than space propulsion.
Document ID
19720030766
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kaufman, H. R.
Cohen, A. J. (NASA Lewis Research Center Cleveland, Ohio, United States)
Date Acquired
August 6, 2013
Publication Date
October 1, 1971
Subject Category
Propulsion Systems
Meeting Information
Meeting: American Physical Society and Brookhaven National Laboratory, Symposium on Ion Sources and Formation of Ion Beams
Location: Upton, NY
Start Date: October 19, 1971
End Date: October 21, 1971
Sponsors: Brookhaven National Laboratory, American Physical Society
Accession Number
72A14432
Distribution Limits
Public
Copyright
Other

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