Plasma Potential Measurements in the Discharge Channel of a 6-kW Hall Thruster

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Topics

• Heating, Ventilating, and Air Conditioning
• Ion Thruster
• Mass Transfer
• Phase Transition
• Propellant
• Propulsion and Power
• Spacecraft Propulsion
• Thermodynamic Process
• Thermodynamic Properties
• Thermodynamics
• Thermophysical Properties
• Thermophysics and Heat Transfer

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Keywords

• Hall Thruster
• Electron Temperature
• Mass Flow Rate
• Plasmadynamics and Electric Propulsion Laboratory
• Hot Cathodes
• Propellant
• Data Acquisition
• Magnetic Field Strength
• Power Supplies
• Satellite Propulsion

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Digital

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Topics

• Joint Propulsion