Modeling Ion propulsion plume interactions with spacecraft in formation flight

This paper presents a simulation study of ion thruster plume effects on formation flying spacecraft. Two formation flight applications using micro-ion propulsion are considered: an L2-Halo orbit interferometer formation and a LEO micro-satellite formation. Worst case scenarios in both missions have...

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Bibliographic Details
Main Authors: Kafafy, Raed, Yong, Cao
Format: Article
Language:English
Published: Royal Aeronautical Society 2010
Subjects:
Online Access:http://irep.iium.edu.my/17253/
http://irep.iium.edu.my/17253/
http://irep.iium.edu.my/17253/4/Modelling_ion_propulsion_plume_interactions.pdf