Multi-scale modeling of ionic electrospray emission
Author:
Affiliation:
1. Department of Astronautical Engineering, University of Southern California, Los Angeles, California 90089, USA
Funder
Air Force Research Laboratory
Publisher
AIP Publishing
Subject
General Physics and Astronomy
Link
https://aip.scitation.org/doi/am-pdf/10.1063/5.0071483
Reference58 articles.
1. Fabrication and characterization of a fully conventionally machined, high-performance porous-media electrospray thruster
2. Characterization of an ionic liquid electrospray thruster with a porous ceramic emitter
3. Characterization of the TILE Electrospray Emitters
4. Environmental and Lifetime Testing of the BET-300-P Electrospray Thruster
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2. Simple model of multi-scale and multi-site emissions for porous ionic liquid electrospray thrusters;Journal of Applied Physics;2024-06-27
3. Study on the plume self-neutralization of ionic liquid electrospray thruster based on median potential;Plasma Sources Science and Technology;2024-05-01
4. Electric-field-induced ion evaporation from the ionic liquid–vacuum interface;Physics of Fluids;2023-12-01
5. Numerical Simulation of Ionic Electrospray Contamination for Small Satellite Formation Flight;IEEE Transactions on Plasma Science;2023-09
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