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Hall Thruster Simulations
Radial-Axial Hybrid Simulations - Related
Papers
Hybrid simulations in the radial-axial plane of an annular Hall
Thruster, based on the model developed by J. M. Fife (MIT, 1998), are
used to study the interior and near-field region of a Hall Thruster
plasma. In the past, these simulations have been used to examine
various phenomena such as channel wall erosion, background pressure,
charge exchange collisions, heavy-particle wall interactions, and
neutral particle injection. Also, measurements of the electron mobility
in a laboratory Hall Thruster have permitted the study of electron
cross-field transport through comparison of simulated discharge
properties using experimentally-measured, Bohm-type, and classical
mobilities. Presently, active areas of interest include the study of
axial resistive instabilities, the use of novel propellants such as
Bismuth and Nitrogen, and the implementation of a time-varying,
calculated electron mobility using an empirical shear-based approach.
Axial-Azimuthal Fluid Simulations - Related
Papers
A high fidelity Hall Thruster simulation has been
formulated in the axial-azimuthal coordinate plane.This numerical model
incorporates the dynamic continuum equations for
the both the electrons and ions and includes the often neglected
contributions of electron momentum and unsteady electron flow.The
coordinate system selected for this simulation, as well as
the inclusion of non-linear electron momentum terms, allows this model
to self
consistently evolve fundamental plasma oscillations in the electron and
ion
fields and predict non-linear wave coupling behavior.The goal of this
research is to understand the connection
between
plasma oscillations and the enhanced electron mobility observed in the
Hall
Thruster.
Simulation of Electron Behavior in Near Field Region - Related
Papers
Axial-Azimuthal Hybrid Simulations (?) - Related
Papers