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Fundamental difference between the two Hall thruster variants
E. Y. Choueiri
Mechanical & Aerospace Engineering
Princeton University
Research output
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Contribution to journal
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Article
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peer-review
74
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Keyphrases
Hall Thruster
100%
Stationary Plasma Thruster
75%
Acceleration Zone
50%
Analytical Model
25%
Insulator
25%
Stainless Steel
25%
Pressure Gradient
25%
Boron Nitride
25%
Secondary Electron Emission
25%
Electronic Energy Loss
25%
Electron Pressure
25%
Repellent
25%
Axial Location
25%
Potential Gradient
25%
Secondary Electron Emission Coefficient
25%
Wall Potential
25%
Higher Secondary
25%
Engineering
Thruster
100%
Hall Thruster
100%
Electron Emission
40%
Secondary Electrons
40%
Electron Energy
40%
Energy Dissipation
20%
Analytical Model
20%
Nitride
20%
Stainless Steel
20%
Axial Location
20%
Potential Gradient
20%
Emission Coefficient
20%
Pressure Gradient
20%
Earth and Planetary Sciences
Hall Thruster
100%
Electron Energy
50%
Stainless Steel
25%
Electron Pressure
25%
Potential Gradient
25%
Nitride
25%
Energy Dissipation
25%
Pressure Gradient
25%
Physics
Hall Thruster
100%
Electron Emission
50%
Electron Energy
50%
Boron Nitride
25%
Pressure Gradient
25%
Material Science
Anode
100%
Boron Nitride
25%
Stainless Steel
25%