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

TitlePolyatomic Ion-Induced Electron Emission (IIEE) in Electrospray Thrusters
Publication TypeJournal Article
Year of Publication2020
AuthorsMagnusson, Jared M., Adam L. Collins, and Richard E. Wirz
JournalAerospace
Volume7
Issue11
Start Page153
Date Published10/2020
ISSN2226-4310
Keywordsdroplet, electrospray, facility effects, ion, kinetic emission, lifetime, molecule, overspray, secondary electron emission
AbstractTo 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 impingement by EMI+ cations becomes significant once EMI+ attains a threshold velocity of ∼9e5 cm/s. The mean secondary electron yield, γ¯, exhibits strong linearity with respect to EMI+ velocity for typical electrospray operating regimes, and we present a simple linear fit equation corresponding to thruster potentials greater than 1 kV. The model chosen for our analysis was shown to be the most appropriate for molecular ion bombardments and is a useful tool in estimating IIEE yields in electrospray devices for molecular ion masses less than ∼1000 u and velocities greater than ∼1e6 cm/s. Droplet-induced electron emission (DIEE) in electrospray thrusters was considered by treating a droplet as a macro-ion, with low charge-to-mass ratio, impacting a solid surface. This approach appears to oversimplify back-spray phenomena, meaning a more complex analysis is required. While semi-empirical models of IIEE, and the decades of solid state theory they are based upon, represent an invaluable advance in understanding secondary electron emission in electrospray devices, further progress would be gained by investigating the complex surfaces the electrodes acquire over their lifetimes and considering other possible emission processes.
URLhttps://www.mdpi.com/2226-4310/7/11/153
DOI10.3390/aerospace7110153

Download File (pdf)

This publication may be downloaded for personal use only. Any other use requires prior permission of the authors and publisher.