Ion-thruster plume modeling for backflow contamination
Author:
Affiliation:
1. Massachusetts Institute of Technology, Cambridge, Massachusetts 02139
2. Worcester Polytechnic Institute, Worcester, Massachusetts 01609
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.26795
Reference33 articles.
1. Electric propulsion flight experience and technology readiness
2. Electron Bombardment Thruster Field and Particle Interfaces
3. Beam efflux measurements for a 30 cm mercury ion thruster
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