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Kinetic simulation of ion thruster plume neutralization in a vacuum chamber
Keita Nishii,
Deborah A. Levin
Aerospace Engineering
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Keyphrases
Plume
100%
Kinetic Simulation
100%
Vacuum Chamber
100%
Ion Thruster Plume
100%
Neutralizer
83%
Background Pressure
33%
Thruster
33%
Chamber Wall
33%
Current Path
33%
Sidewall
16%
Direct Simulation Monte Carlo
16%
High Background
16%
Electron Temperature
16%
Ion Current
16%
Electric Potential
16%
High-performance Simulation
16%
Xenon
16%
Testing Environment
16%
Test Chamber
16%
Beam Ions
16%
Experimental Testing
16%
Relative Potential
16%
Plasma Flow
16%
Particle-in-cell Simulation
16%
Ground Experiment
16%
Potential Temperature
16%
Charge-exchange Ions
16%
Gridded Ion Thruster
16%
Facility Effects
16%
Ion Sheath
16%
Electrical Microenvironment
16%
Vacuum Testing
16%
Physics
Electron Energy
100%
Ion Current
100%
Electric Potential
100%
Potential Temperature
100%
Blood Plasma
100%
Monte Carlo Method
100%
Electron Beam
100%
Ion Beam
100%