Polyatomic Ion-Induced Electron Emission (IIEE) in Electrospray Thrusters

To better characterize the lifetime and performance of electrospray thrusters, electron emission due to electrode impingement by the propellant cation 1-ethyl-3-methylimidazolium (EMI+) has been evaluated with semi-empirical modeling techniques. Results demonstrate that electron emission due to grid...

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Bibliographic Details
Main Authors: Jared M. Magnusson, Adam L. Collins, Richard E. Wirz
Format: Article
Language:English
Published: MDPI AG 2020-10-01
Series:Aerospace
Subjects:
Online Access:https://www.mdpi.com/2226-4310/7/11/153