Experiments were undertaken to determine sputter yields of potential ion beam target materials, to assess the impact of charge exchange on beam diagnostics in large facilities, and to examine material erosion and deposition after a 957 hr test of a 5 kW-class ion thruster. The xenon ion sputter yield of flexible graphite was lower than other graphite forms especially at high angles of incidence. Ion beam charge exchange effects were found to hamper beam probe current collection diagnostics even at pressures from 0.7 to 1.7 mPa. Estimates of the xenon ion beam envelope were made and predictions of the thickness of sputter deposited coatings in the facility were compared with measurements
A survey of low energy xenon ion impact sputter yields was conducted to provide a more coherent base...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76408/1/AIAA-2001-3353-473.pd
Ion thruster engines for spacecraft propulsion can serve as ion beam sources for potential space pro...
Tests were performed to establish 30-cm ion thruster plume impacts, including plume characterization...
Ion propulsion research and development yields a mature technology that is transferable to a wide ra...
A simple model for the production of ions that impinge on and sputter erode the accelerator grid of ...
In this paper, we describe a technique that was used to measure total and differential sputter yield...
Ion thrusters offer the potential to enable many future interplanetary robotic missions presently un...
Sputter erosion in ion thrusters has been measured in lifetests at discharge voltages as low as 25 V...
The general operation of a discharge chamber for the production of ions is described. A model is pre...
Proposed solutions to the problems of sputter erosion and sputtered material spalling in the dischar...
A 5 cm diameter mercury ion thruster similar to one tested for 9715 hours was operated approximately...
Sputtering and deposition rates were measured for discharge chamber components of a 30-cm diameter m...
Results of an experimental study of the characteristics of ion thruster hollow cathodes operating at...
The work performed on the Ion Propulsion System Technology Task in FY90 is described. The objectives...
A survey of low energy xenon ion impact sputter yields was conducted to provide a more coherent base...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76408/1/AIAA-2001-3353-473.pd
Ion thruster engines for spacecraft propulsion can serve as ion beam sources for potential space pro...
Tests were performed to establish 30-cm ion thruster plume impacts, including plume characterization...
Ion propulsion research and development yields a mature technology that is transferable to a wide ra...
A simple model for the production of ions that impinge on and sputter erode the accelerator grid of ...
In this paper, we describe a technique that was used to measure total and differential sputter yield...
Ion thrusters offer the potential to enable many future interplanetary robotic missions presently un...
Sputter erosion in ion thrusters has been measured in lifetests at discharge voltages as low as 25 V...
The general operation of a discharge chamber for the production of ions is described. A model is pre...
Proposed solutions to the problems of sputter erosion and sputtered material spalling in the dischar...
A 5 cm diameter mercury ion thruster similar to one tested for 9715 hours was operated approximately...
Sputtering and deposition rates were measured for discharge chamber components of a 30-cm diameter m...
Results of an experimental study of the characteristics of ion thruster hollow cathodes operating at...
The work performed on the Ion Propulsion System Technology Task in FY90 is described. The objectives...
A survey of low energy xenon ion impact sputter yields was conducted to provide a more coherent base...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76408/1/AIAA-2001-3353-473.pd
Ion thruster engines for spacecraft propulsion can serve as ion beam sources for potential space pro...