Quantifying Uncertainty in Predictions of Spacecraft Erosion Induced by a Hall Thruster
Author:
Affiliation:
1. University of Michigan, Ann Arbor, Michigan 48109
2. University of Colorado Boulder, Boulder, Colorado 80309
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.A35196
Reference29 articles.
1. Modeling of Stationary Plasma Thruster-100 Thruster Plumes and Implications for Satellite Design
2. End-of-life Stationary Plasma Thruster far-field plume characterization
3. Far-field plume contamination and sputtering of the stationary plasma thruster
4. Interactions Between Spacecraft and Thruster Plumes
5. Spacecraft Charging, Plume Interactions, and Space Radiation Design Considerations for All-Electric GEO Satellite Missions
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