Open AccessEffects of Enhanced Eathode Electron Emission on Hall Thruster Operation
Author(s) -
A. Smirnov and N. J. Fisch Y. Raitses
Publication year - 2009
Language(s) - English
Resource type - Reports
DOI - 10.2172/953211
Subject(s) - electron , magnetic field , plasma , cathode , physics , hall effect , atomic physics , field electron emission , field (mathematics) , aerospace engineering , electrical engineering , engineering , nuclear physics , mathematics , quantum mechanics , pure mathematics
Interesting discharge phenomena are observed that have to do with the interaction between the magnetized Hall thruster plasma and the neutralizing cathode. The steadystate parameters of a highly ionized thruster discharge are strongly influenced by the electron supply from the cathode. The enhancement of the cathode electron emission above its self-sustained level affects the discharge current and leads to a dramatic reduction of the plasma divergence and a suppression of large amplitude, low frequency discharge current oscillations usually related to an ionization instability. These effects correlate strongly with the reduction of the voltage drop in the region with the fringing magnetic field between the thruster channel and the cathode. The measured changes of the plasma properties suggest that the electron emission affects the electron cross-field transport in the thruster discharge. These trends are generalized for Hall thrusters of various configurations