The importance of the cathode plume and its interactions with the ion beam in numerical simulations of Hall thrusters
Author:
Affiliation:
1. Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California 91109, USA
Funder
Jet Propulsion Laboratory (JPL)
Publisher
AIP Publishing
Subject
Condensed Matter Physics
Link
http://aip.scitation.org/doi/pdf/10.1063/1.4947554
Reference46 articles.
1. M. Hirakawa and Y. Arakawa , “ Numerical simulation of plasma particle behavior in a Hall thrusters,” AIAA Paper No. 96-3195.
2. Study of stationary plasma thrusters using two-dimensional fully kinetic simulations
3. J. J. Szabo , “ Fully kinetic numerical modeling of a plasma thruster,” Ph.D. thesis ( Massachusetts Institute of Technology, 2001).
4. J. M. Fife , Ph.D. thesis ( Massachusetts Institute of Technology, 1998).
5. A two-dimensional hybrid model of the Hall thruster discharge
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