Modelling 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...

Full description

Bibliographic Details
Main Authors: Kafafy, Raed Ismail, Cao, Y.
Format: Article
Language:English
Published: Royal Aeronautical Society 2010
Subjects:
Online Access:http://irep.iium.edu.my/11900/
http://irep.iium.edu.my/11900/
http://irep.iium.edu.my/11900/1/modelling_ion_propulsion.pdf

Similar Items