DocumentCode :
2072892
Title :
Xe ion plasma thruster XIPS-200 for orbit correction of geostationary communication satellite
Author :
Stepanushkin, N.P. ; Koshelev, N.N. ; Aliyeva, M.T. ; Loyan, A.V. ; Ishenko, E.I.
Author_Institution :
Nat. Aerosp. Univ., Kharkov, Ukraine
fYear :
2005
fDate :
9-11 June 2005
Firstpage :
355
Lastpage :
357
Abstract :
One of the more developed, approbate in space condition, reliable and having big work resources electric propulsions (EP) is ion plasma thruster (IPT). Probably therefore for today it is in demand for solution of broad-spectrum tasks of space vehicles movement. One of them is orbit correction of weighty geostationary communication satellites.
Keywords :
aerospace engines; artificial satellites; ion engines; xenon; IPT; XIPS-200; Xe ion plasma thruster; geostationary communication satellite; orbit correction; space vehicles movement; Aerospace testing; Anodes; Artificial satellites; Boring; Brightness; Cathodes; DC generators; Electrodes; Electrons; Plasmas;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Recent Advances in Space Technologies, 2005. RAST 2005. Proceedings of 2nd International Conference on
Print_ISBN :
0-7803-8977-8
Type :
conf
DOI :
10.1109/RAST.2005.1512591
Filename :
1512591
Link To Document :
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