Plasma interaction with emmissive surface with Debye-scale grooves
Author:
Funder
Air Force Office of Scientific Research
Russian Science Foundation
Publisher
IOP Publishing
Subject
Condensed Matter Physics
Link
http://iopscience.iop.org/article/10.1088/1361-6595/aab6d8/pdf
Reference18 articles.
1. Plasma flow and plasma–wall transition in Hall thruster channel
2. Wall material effects in stationary plasma thrusters. I. Parametric studies of an SPT-100
3. Wall material effects in stationary plasma thrusters. II. Near-wall and in-wall conductivity
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1. Plasma–Wall Interaction Model for Erosion of Materials Under Ion Bombardment;Journal of Propulsion and Power;2023-05
2. Wear trends of the 12.5 kW HERMeS Hall thruster;Journal of Applied Physics;2021-10-14
3. Plasma sheath material induced dependence due to secondary electron emission;Physics of Plasmas;2020-04
4. Genesis of non-uniformity of plasma fluxes over emissive wall in low-temperature plasmas;Plasma Research Express;2019-12-03
5. Latest progress in Hall thrusters plasma modelling;Reviews of Modern Plasma Physics;2019-07-18
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