This paper reports on a field-emission cathode for use in electric propulsion that has the potential for very long lifetime due to its ability to be regenerated when the emitter tip(s) become damaged. The field-emitting tips were formed by applying an ion-extracting electric potential to a heated indium-coated tungsten needle, known as a liquidmetal ion source. The liquid-metal ion source was then cooled, freezing in a solid nanotip at the apex. When the modified emitter was then subjected to electron-extracting potentials, stable and long-lived electron emission was observed. The first goal of this investigation was to operate and quench a liquid-metal ion source at ion emission currents from 1 to 30 μA to acquire micrographs of the surfac...
In liquid metal ion sources, the emission is located at the apex of a liquid cone (the often so-call...
Field emission from the electrodes of practical electron guns is one of the principal phenomena limi...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76844/1/AIAA-2005-3663-570.pd
This research investigates the discharge characteristics of a field emission cathode for use in elec...
The research reported here focuses on the surface topography of a field-emission cathode for use in ...
The research reported here focuses on the surface topography of a field-emission cathode for use in ...
This research investigates the discharge characteristics of a field emission cathode for use in elec...
The research reported here focuses on the surface topography of a field-emission cathode for use in ...
The research reported here explores the possibility of field-emission cathodes for use in EP that ha...
This research investigates the discharge characteristics of a field-emission cathode for use in Elec...
Field emission cathodes have been considered for use as neutralizers on electric propulsion systems....
LGEP 2014 ID = 1593International audienceThe effect of stainless steel cathode surface morphology on...
Spindt-type field-emission cathodes for use in electric propulsion (EP) systems having self-assembli...
A self-regenerative field emission source was demonstrated. The emission source (cathode) consisted ...
Field emission is one of the principal phenomena limiting the operating voltage of practical electro...
In liquid metal ion sources, the emission is located at the apex of a liquid cone (the often so-call...
Field emission from the electrodes of practical electron guns is one of the principal phenomena limi...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76844/1/AIAA-2005-3663-570.pd
This research investigates the discharge characteristics of a field emission cathode for use in elec...
The research reported here focuses on the surface topography of a field-emission cathode for use in ...
The research reported here focuses on the surface topography of a field-emission cathode for use in ...
This research investigates the discharge characteristics of a field emission cathode for use in elec...
The research reported here focuses on the surface topography of a field-emission cathode for use in ...
The research reported here explores the possibility of field-emission cathodes for use in EP that ha...
This research investigates the discharge characteristics of a field-emission cathode for use in Elec...
Field emission cathodes have been considered for use as neutralizers on electric propulsion systems....
LGEP 2014 ID = 1593International audienceThe effect of stainless steel cathode surface morphology on...
Spindt-type field-emission cathodes for use in electric propulsion (EP) systems having self-assembli...
A self-regenerative field emission source was demonstrated. The emission source (cathode) consisted ...
Field emission is one of the principal phenomena limiting the operating voltage of practical electro...
In liquid metal ion sources, the emission is located at the apex of a liquid cone (the often so-call...
Field emission from the electrodes of practical electron guns is one of the principal phenomena limi...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76844/1/AIAA-2005-3663-570.pd