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Parametric studies of the Hall current plasma thruster
J. Ashkenazy
,
Y. Raitses
, G. Appelbaum
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:
Contribution to journal
›
Article
›
peer-review
40
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Keyphrases
Hall Current
100%
Thruster
100%
Rocket Engine
100%
Plasma Thruster
100%
Hall Thruster
50%
Magnetic Field
50%
Operating Conditions
50%
Gas Flow Rate
50%
Electrical Characteristics
50%
Applied Voltage
50%
Acceleration Mechanism
50%
Jet Velocity
50%
Channel Length
50%
Channel Material
50%
Radial Magnetic Field
50%
Channel Geometry
50%
Axial Electric Field
50%
Wall Material
50%
Space Charge Effect
50%
Configuration Variation
50%
Gas Flow Rate Measurement
50%
Plasma Diagnostics
50%
Magnetic Imaging
50%
Large-current-density
50%
Plasma Jet
50%
Channel Walls
50%
Small Rocket
50%
Electrical Diagnosis
50%
Optimal Channels
50%
Engineering
Thruster
100%
Parametric Study
100%
Magnetic Field
50%
Gas Flowrate
50%
Rocket Engine
50%
Flow Rate
25%
Hall Thruster
25%
Space Charge
25%
Applied Voltage
25%
Jet Velocity
25%
Channel Length
25%
Channel Wall
25%
Channel Geometry
25%
Plasma Diagnostics
25%
Flow Velocity
25%
Electric Field
25%
Jet
25%
Spacecraft
25%