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<sup>+</sup>) has been evaluated with semi-empirical modeling techniques. Results demonstrate that electr...

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Bibliographic Details
Published in:Aerospace
Main Authors: Jared M. Magnusson, Adam L. Collins, Richard E. Wirz
Format: Article
Language:English
Published: MDPI AG 2020-10-01
Subjects:
electrospray
lifetime
overspray
secondary electron emission
facility effects
kinetic emission
Online Access:https://www.mdpi.com/2226-4310/7/11/153

Internet

https://www.mdpi.com/2226-4310/7/11/153

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