NASA NTRS · 19720030766
Maximum propellant utilization in an electron-bombardment thruster.
Abstract
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.
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Kaufman, H. R., Cohen, A. J.. 1971-10-01. Maximum propellant utilization in an electron-bombardment thruster.. https://ntrs.nasa.gov/citations/19720030766
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