Numerical study of spacecraft contamination and interactions by ion-thruster effluents
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/10.2514/3.26796
Reference8 articles.
1. 2SamantaRoy, R. I. "Numerical Simulation of Ion Thruster Plume Backflow for Spacecraft Contamination Assessment," Ph.D. Thesis,Dept. of Aeronautics and Astronautics, Massachusetts Inst. of Technology, Cambridge, MA,June 1995.
2. NASA 30 cm ion thruster development status
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