Langmuir Probe Studies of Magnetic Confinement in an Ion Thruster Discharge Plasma
Author:
Affiliation:
1. Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California 91109
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.36547
Reference22 articles.
1. Analytical Ion Thruster Discharge Performance Model
2. 2-D Discharge Chamber Model for Ion Thrusters
3. LaB6 Hollow Cathodes for Ion and Hall Thrusters
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