Erosion of the acceleration channel is the main lifetime limiting factor for Hall Effect Thrusters (HETs). Impacting ions damage the wall insulation that protects the magnetic circuitry from the plasma. To improve HET technology, it is necessary to simulate plasma behavior inside the channel, and associated erosion rates. This work presents a 2-dimensional Particle-in-Cell model, developed to predict channel wall erosion in Hall thrusters, using an SPT-100 as reference thruster, and providing estimations in good agreement with experimental values. The model allows for evaluation of different erosion mechanisms, both combined as individually. From different simulation results, erosion due to the sheath conditions has proven to be the dominan...
Hall thruster lifetime codes presently under development at NASA aim to provide predictive tools tha...
This dissertation describes the use of optical diagnostics to study the Hall thruster channel wall e...
In a Qualification Life Test (QLT) of the BPT-4000 Hall thruster that recently accumulated greater t...
Erosion of the acceleration channel is the main lifetime limiting factor for Hall Effect Thrusters (...
Lifetime issues for Hall thrusters are becoming increasingly important as the mission envelopes for ...
Hall Thruster degradation due to wall sputtering by heavy particle bombardment is assessed by develo...
A simple analytic model predicted Hall thruster channel erosion based on thruster geometry, operatin...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76799/1/AIAA-2005-3530-604.pd
The most common type of electric propulsion in space exploration is the Hall Effect Thruster (HET), ...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76234/1/AIAA-2006-4657-608.pd
International audienceHall effect thrusters (HET) are one of the main technology used and studied fo...
One of the challenges facing further utilization of Hall thrusters for space missions is establishin...
The primary life-limiting mechanism of Hall thrusters is the sputter erosion of the discharge channe...
Hall thrusters, a type of space electric propulsion, offer high specific impulses attractive for a v...
Thesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 201...
Hall thruster lifetime codes presently under development at NASA aim to provide predictive tools tha...
This dissertation describes the use of optical diagnostics to study the Hall thruster channel wall e...
In a Qualification Life Test (QLT) of the BPT-4000 Hall thruster that recently accumulated greater t...
Erosion of the acceleration channel is the main lifetime limiting factor for Hall Effect Thrusters (...
Lifetime issues for Hall thrusters are becoming increasingly important as the mission envelopes for ...
Hall Thruster degradation due to wall sputtering by heavy particle bombardment is assessed by develo...
A simple analytic model predicted Hall thruster channel erosion based on thruster geometry, operatin...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76799/1/AIAA-2005-3530-604.pd
The most common type of electric propulsion in space exploration is the Hall Effect Thruster (HET), ...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76234/1/AIAA-2006-4657-608.pd
International audienceHall effect thrusters (HET) are one of the main technology used and studied fo...
One of the challenges facing further utilization of Hall thrusters for space missions is establishin...
The primary life-limiting mechanism of Hall thrusters is the sputter erosion of the discharge channe...
Hall thrusters, a type of space electric propulsion, offer high specific impulses attractive for a v...
Thesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 201...
Hall thruster lifetime codes presently under development at NASA aim to provide predictive tools tha...
This dissertation describes the use of optical diagnostics to study the Hall thruster channel wall e...
In a Qualification Life Test (QLT) of the BPT-4000 Hall thruster that recently accumulated greater t...