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Pelaez Alvarez, Jesus and Sanjurjo Rivo, Manuel and Scheeres, D.J. (2009). Jovian capture of a spacecraft with a self-balanced electrodynamic bare tether. In: "19th AAS/AIAA Space Flight Mechanics Meeting", 8-12 feb 2009, Savannah, Georgia. pp. 2141-2160.
Title: | Jovian capture of a spacecraft with a self-balanced electrodynamic bare tether |
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Author/s: |
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Item Type: | Presentation at Congress or Conference (Article) |
Event Title: | 19th AAS/AIAA Space Flight Mechanics Meeting |
Event Dates: | 8-12 feb 2009 |
Event Location: | Savannah, Georgia |
Title of Book: | Space Flight Mechanics 2009 . Advances in Astronautical Sciences |
Date: | 2009 |
Volume: | 134 |
Subjects: | |
Faculty: | E.T.S.I. Aeronáuticos (UPM) |
Department: | Aeronaves y Vehículos Espaciales |
Creative Commons Licenses: | Recognition - No derivative works - Non commercial |
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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
Type | Code | Acronym | Leader | Title |
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Government of Spain | ESP2007-64068 | Unspecified | Unspecified | Propagation of Orbits, Advanced Orbital Dynamics and Use of Space Tethers |
Item ID: | 52186 |
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DC Identifier: | https://oa.upm.es/52186/ |
OAI Identifier: | oai:oa.upm.es:52186 |
Official URL: | http://www.space-flight.org/AAS_meetings/2009_winter/2009%20winter.html |
Deposited by: | Memoria Investigacion |
Deposited on: | 26 Mar 2019 10:49 |
Last Modified: | 26 Mar 2019 10:49 |