DocumentCode :
3189286
Title :
Characteristic Properties of Deorbiting of an Electrodynamic Two Cubesat Tether in a Near-polar Orbit
Author :
Khoroshilov, V.S. ; Pirozhenko, A.V. ; Zakrzhevskii, A.E.
Author_Institution :
State Design Office "Pivdenne", Dnepropetrovsk
fYear :
2007
fDate :
14-16 June 2007
Firstpage :
176
Lastpage :
181
Abstract :
Features of equilibrium condition of an electrodynamic two bodies tether of small mass are investigated in near-polar orbit. Change of such characteristic parameters, as tension of the tether, radius of its curvature, angle of deviation from the orbital plane, induced e.m.f. and others is traced during the day. The problem duration of lifetime of the tether in a near-earth circular orbit is considered.
Keywords :
Earth orbit; aerospace instrumentation; artificial satellites; electromagnetic forces; de orbiting; electrodynamic cubesat tether; eletromagnetic force; near-Earth circular orbit; near-polar orbit; orbital plane; tension; Conductors; Current; Earth; Electrodynamics; Electrons; Kinetic energy; Magnetic fields; Plasmas; Power engineering and energy; Space vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Recent Advances in Space Technologies, 2007. RAST '07. 3rd International Conference on
Conference_Location :
Istanbul
Print_ISBN :
1-4244-1057-6
Electronic_ISBN :
1-4244-1057-6
Type :
conf
DOI :
10.1109/RAST.2007.4283972
Filename :
4283972
Link To Document :
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