Interior and Near-Wall Ion Velocity Distribution Functions in the H6 Hall Thruster
Author:
Affiliation:
1. Plasmadynamics and Electric Propulsion Laboratory, University of Michigan, Ann Arbor, Michigan 48109
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.B34712
Reference31 articles.
1. Predicting Hall Thruster Operational Lifetime
2. An Investigation of Factors Involved in Hall Thruster Wall Erosion Modeling
3. Simulating Plasma-Induced Hall Thruster Wall Erosion With a Two-Dimensional Hybrid Model
4. Low-energy xenon ion sputtering of ceramics investigated for stationary plasma thrusters
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