Excessive cross-field electron mobility in Hall thrusters has a negative effect on thruster efficiency and has been shown experimentally to be much larger than predicted by classical collisional transport theory. An electron trapping apparatus was constructed at Michigan Tech’s Isp Lab in order to study electron dynamics in the defining electric and magnetic fields of a Hall-effect thruster. This apparatus was designed to stably trap a non-neutral electron plasma in a confining volume in order to study these dynamics in a highly controlled environment. Electrons are confined using only electric and magnetic fields in the absence of ions and dielectric walls, which are present in a typical Hall thruster. Mobility studies on a low-density, no...
Neutral flow dynamics in Hall thrusters are not often regarded as a critical aspect that controls th...
In an effort to understand the role of neutral flow dynamics in the operation of Hall thrusters, a f...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76339/1/AIAA-2005-4057-695.pd
An electron-trapping apparatus was constructed to study electron dynamics in the defining fields of ...
An electron trapping apparatus was constructed in order to study electron dynamics in the defining e...
An electron trapping apparatus was constructed in order to study electron dynamics in the defining e...
A two-dimensional hybrid particle-in-cell numerical model has been constructed in the radial-axial p...
Stable operation of a Hall thruster that emits and collects the Hall current across a planar dischar...
This paper presents the observation of an electron mobility mechanism in Hall thruster fields that c...
A Hall thruster, an E × B device used for in-space propulsion, utilizes an axial electric field to e...
Axial electron transport represents a loss in efficiency for crossed field devices, such as Hall-eff...
International audienceUsing a 1D particle-in-cell simulation with perpendicular electric, E0, and ma...
Measurements of the turbulent magnetic field in a Hall thruster have been carried out between 1 kHz ...
International audienceMeasurements of the turbulent magnetic field in a Hall thruster have been carr...
The role of electron-wall collisions in Hall thruster operation is studied through simulation of the...
Neutral flow dynamics in Hall thrusters are not often regarded as a critical aspect that controls th...
In an effort to understand the role of neutral flow dynamics in the operation of Hall thrusters, a f...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76339/1/AIAA-2005-4057-695.pd
An electron-trapping apparatus was constructed to study electron dynamics in the defining fields of ...
An electron trapping apparatus was constructed in order to study electron dynamics in the defining e...
An electron trapping apparatus was constructed in order to study electron dynamics in the defining e...
A two-dimensional hybrid particle-in-cell numerical model has been constructed in the radial-axial p...
Stable operation of a Hall thruster that emits and collects the Hall current across a planar dischar...
This paper presents the observation of an electron mobility mechanism in Hall thruster fields that c...
A Hall thruster, an E × B device used for in-space propulsion, utilizes an axial electric field to e...
Axial electron transport represents a loss in efficiency for crossed field devices, such as Hall-eff...
International audienceUsing a 1D particle-in-cell simulation with perpendicular electric, E0, and ma...
Measurements of the turbulent magnetic field in a Hall thruster have been carried out between 1 kHz ...
International audienceMeasurements of the turbulent magnetic field in a Hall thruster have been carr...
The role of electron-wall collisions in Hall thruster operation is studied through simulation of the...
Neutral flow dynamics in Hall thrusters are not often regarded as a critical aspect that controls th...
In an effort to understand the role of neutral flow dynamics in the operation of Hall thrusters, a f...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76339/1/AIAA-2005-4057-695.pd