An electron emitter neutraliser to prevent spacecraft charging from the use of positive ion thrusters is under development at the Rutherford Appleton Laboratory. A particle-in-cell code, KARAT, has been used to simulate laboratory experiments, Laboratory test results have been successfully obtained with simulations, for model verification. Neutraliser-ion thruster interactions in space have also been modelled. An ion-propelled spacecraft rapidly charges to kilovolt potentials, which can be dissipated by an electron-emitting neutraliser. The effect of background particle concentrations on neutralisation has also been studied
The radiation environment in space is very different from the one encountered on Earth. In addition ...
Design of the next generation of ion engines can benefit from detailed computer simulations of the p...
The Neutralized Transport Experiment (NTX) at Lawrence Berkeley National Laboratory has been designe...
An electron emitter neutraliser to prevent spacecraft charging from the use of positive ion thruster...
Electric space propulsion is superior to conventional chemical systems because of its greatly enhanc...
Active (i.e. deliberate) electron emission in space is a powerful scientific technique that often pr...
The experimental ion-beam behavior obtained without neutralizers is compared with both simple collis...
Neutralization of the ion beam produced by a FEEP thruster is in principle a task similar to the wel...
This paper presents a simulation study of ion thruster plume effects on formation flying spacecraft....
Electric propulsion thrusters considerable modify the plasma environment around a spacecraft. Charge...
Experiments are under way to investigate the extent to which various space charge neutralization met...
The focus of this research is to explore technologies for enabling the use of molecular propellants ...
A numerical model of the ion beam in field emission electric propulsion thrusters is presented. The ...
For the transport of high-intensity hadron beams in low-energy beam lines of linear accelerators, th...
Neutralization test data obtained on the SERT 2 spacecraft are presented. Tests included ion beam ne...
The radiation environment in space is very different from the one encountered on Earth. In addition ...
Design of the next generation of ion engines can benefit from detailed computer simulations of the p...
The Neutralized Transport Experiment (NTX) at Lawrence Berkeley National Laboratory has been designe...
An electron emitter neutraliser to prevent spacecraft charging from the use of positive ion thruster...
Electric space propulsion is superior to conventional chemical systems because of its greatly enhanc...
Active (i.e. deliberate) electron emission in space is a powerful scientific technique that often pr...
The experimental ion-beam behavior obtained without neutralizers is compared with both simple collis...
Neutralization of the ion beam produced by a FEEP thruster is in principle a task similar to the wel...
This paper presents a simulation study of ion thruster plume effects on formation flying spacecraft....
Electric propulsion thrusters considerable modify the plasma environment around a spacecraft. Charge...
Experiments are under way to investigate the extent to which various space charge neutralization met...
The focus of this research is to explore technologies for enabling the use of molecular propellants ...
A numerical model of the ion beam in field emission electric propulsion thrusters is presented. The ...
For the transport of high-intensity hadron beams in low-energy beam lines of linear accelerators, th...
Neutralization test data obtained on the SERT 2 spacecraft are presented. Tests included ion beam ne...
The radiation environment in space is very different from the one encountered on Earth. In addition ...
Design of the next generation of ion engines can benefit from detailed computer simulations of the p...
The Neutralized Transport Experiment (NTX) at Lawrence Berkeley National Laboratory has been designe...