The electron mobility profile is estimated in a 4.5 kW commercial Hall thruster as a function of discharge power. Internal measurements of plasma potential and electron temperature are made in the thruster channel with a high-speed translating probe. These measurements are presented for a range of throttling conditions from 150 - 400 V and 0.6 - 4.5 kW. The fluid-based solver, Hall2De, is used in conjunction with these internal plasma parameters to estimate the anomalous collision frequency profile at fixed voltage, 300 V, and three power levels. It is found that the anomalous collision frequency profile does not change significantly upstream of the location of the magnetic field peak but that the extent and magnitude of the anomalous colli...
The role of electron-wall collisions in Hall thruster operation is studied through simulation of the...
Measurements with a movable emissive probe in a 2 kW Hall thruster revealed several interesting phen...
Stable operation of a Hall thruster that emits and collects the Hall current across a planar dischar...
International audienceMeasurements of the turbulent magnetic field in a Hall thruster have been carr...
Measurements of the turbulent magnetic field in a Hall thruster have been carried out between 1 kHz ...
Accurate modeling of the anomalous electron mobility is crucial for successful simulation of Hall th...
The discharge current oscillation at a frequency range of 10–100 kHz in Hall thrusters was investiga...
In an effort to understand the role of neutral flow dynamics in the operation of Hall thrusters, a f...
A quasi one-dimensional (1-D) steady-state model of the Hall thruster is presented. For the same dis...
During the early development stages of Hall thruster technology, plasma research and propulsion adva...
An experimental investigation is presented to quantify the effect of high-speed probing on the plasm...
Characteristics of plasma fluctuations at the frequencies 10–100 kHz in Hall thrusters were investig...
The Plasmadynamics and Electric Propulsion Laboratory High-speed Axial Reciprocating Probe system is...
A quasi one-dimensional steady-state model of the Hall thruster is presented. For given mass flow ra...
Electron-wall interaction effects in Hall thrusters are studied through measurements of the plasma r...
The role of electron-wall collisions in Hall thruster operation is studied through simulation of the...
Measurements with a movable emissive probe in a 2 kW Hall thruster revealed several interesting phen...
Stable operation of a Hall thruster that emits and collects the Hall current across a planar dischar...
International audienceMeasurements of the turbulent magnetic field in a Hall thruster have been carr...
Measurements of the turbulent magnetic field in a Hall thruster have been carried out between 1 kHz ...
Accurate modeling of the anomalous electron mobility is crucial for successful simulation of Hall th...
The discharge current oscillation at a frequency range of 10–100 kHz in Hall thrusters was investiga...
In an effort to understand the role of neutral flow dynamics in the operation of Hall thrusters, a f...
A quasi one-dimensional (1-D) steady-state model of the Hall thruster is presented. For the same dis...
During the early development stages of Hall thruster technology, plasma research and propulsion adva...
An experimental investigation is presented to quantify the effect of high-speed probing on the plasm...
Characteristics of plasma fluctuations at the frequencies 10–100 kHz in Hall thrusters were investig...
The Plasmadynamics and Electric Propulsion Laboratory High-speed Axial Reciprocating Probe system is...
A quasi one-dimensional steady-state model of the Hall thruster is presented. For given mass flow ra...
Electron-wall interaction effects in Hall thrusters are studied through measurements of the plasma r...
The role of electron-wall collisions in Hall thruster operation is studied through simulation of the...
Measurements with a movable emissive probe in a 2 kW Hall thruster revealed several interesting phen...
Stable operation of a Hall thruster that emits and collects the Hall current across a planar dischar...