DocumentCode :
2444413
Title :
Electron kinetic effects and beam related instabilities in Hall thrusters
Author :
Sydorenko, Dmytro ; Smolyakov, Andrei ; Kaganovich, Igor ; Raitses, Yevgeny
Author_Institution :
Dept. of Phys. & Eng. Phys., Univ. of Saskatchewan, Saskatoon, SK
fYear :
2008
fDate :
15-19 June 2008
Firstpage :
1
Lastpage :
1
Abstract :
Recent analytical studies and particle-in-cell simulations suggested that the electron velocity distribution function in a Hall thruster plasma is non-Maxwellian and anisotropic. The electron average kinetic energy in the direction parallel to walls is several times larger than the electron average kinetic energy in direction normal to the walls. Electrons are stratified into several groups depending on their origin (e.g., plasma discharge volume or thruster channel walls) and confinement (e.g., lost on the walls or trapped in the plasma). Practical analytical formulas are derived for wall fluxes, secondary electron fluxes, plasma parameters and conductivity. The calculations based on analytical formulas agree well with the results of numerical simulations. The self-consistent analysis demonstrates that elastic electron scattering on collisions with atoms and ions plays a key role in formation of the electron velocity distribution function and plasma-wall interaction. The fluxes of electrons from the plasma bulk are shown to be proportional to the rate of scattering to loss cone, thus collision frequency determines the wall potential and secondary electron fluxes. Secondary electron emission from the walls is shown to enhance the electron conductivity across the magnetic field, while having almost no effect on insulating properties of the near-wall sheaths. Such a self-consistent decoupling between secondary electron emission effects on electron energy losses and electron crossed-field transport is currently not captured by the existing fluid and hybrid models of the Hall thrusters. The sheath near the electron-emitting surface may become unstable if it is characterized by the negative volt-ampere characteristics, which occurs in presence of strong secondary electron emission. It is found that in stable stationary plasma state the final phase of cyclotron rotation of secondary electrons emitted from the thruster walls is not arbitrary but belongs to the discrete set- - of stability intervals. In the limit of high discharge voltages, a new regime with relaxation oscillations is identified. In this regime, the plasma constantly switches between a state with non-space charge limited emission and a state with a space charge limited emission.
Keywords :
atom-electron collisions; discharges (electric); energy loss of particles; plasma confinement; plasma instability; plasma kinetic theory; plasma sheaths; plasma transport processes; plasma-wall interactions; secondary electron emission; space-charge-limited conduction; Hall thruster; analytical formula; atom collisions; beam-related instability; collision frequency; cyclotron rotation; elastic electron scattering; electron conductivity; electron crossed-field transport; electron energy loss; electron kinetic effects; electron velocity distribution function; ion collisions; near-wall sheath; nonspace charge limited emission; plasma conductivity; plasma confinement; plasma discharge; plasma parameters; plasma-wall interaction; relaxation oscillation; secondary electron emission; secondary electron flux; self-consistent analysis; space charge limited emission; wall flux; wall potential; Conductivity; Distribution functions; Electron beams; Electron emission; Kinetic energy; Kinetic theory; Particle scattering; Plasma confinement; Plasma simulation; Plasma stability;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Plasma Science, 2008. ICOPS 2008. IEEE 35th International Conference on
Conference_Location :
Karlsruhe
ISSN :
0730-9244
Print_ISBN :
978-1-4244-1929-6
Electronic_ISBN :
0730-9244
Type :
conf
DOI :
10.1109/PLASMA.2008.4591157
Filename :
4591157
Link To Document :
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