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Descripción
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| The exploration of Jupiter and the Jovian system is severely restricted by the scarcity of power, the most limiting factor of scientific missions. Electrodynamic tethers has been proposed as an efficient solution to provide power to the spacecraft. Furthermore, they are pointed out as suitable propulsive devices to perform orbit manoeuvres in the Jovian world. In this paper, the Jovian capture of a spacecraft using a self-balanced electrodynamic tether is analyzed in detail. Different models of current collection are used. A dynamic description of the evolution from the arrival hyperbolic to the final ¿captured¿ orbit is carried out. 2 | |
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Internacional
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Si |
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Nombre congreso
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The 19th AAS/AIAA Spaceflight Mechanics Meeting |
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Tipo de participación
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960 |
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Lugar del congreso
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Savannah, Georgia |
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Revisores
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Si |
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ISBN o ISSN
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1081-6003 |
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DOI
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Fecha inicio congreso
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08/02/2009 |
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Fecha fin congreso
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12/02/2009 |
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Desde la página
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0 |
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Hasta la página
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0 |
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Título de las actas
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Published for the American Astronautical Society by Univelt, Incorporated, P.O. Box 28130, San Diego, California 92198 Web Site: http://www.univelt.com Printed and Bound in the U.S.A. |