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Space Station Reboost with Electrodynamic TethersThis paper presents the results of a study of an electrodynamic tether system to reboost the International Space Station (ISS). One recommendation is to use a partially bare tether for electron collection. Locations are suggested as to where the tether system is to be attached at the space station. The effects of the tether system on the microgravity environment may actually be beneficial, because the system can neutralize aerodrag during quiescent periods and, if deployed from a movable boom, can permit optimization of laboratory positioning with respect to acceleration contours. Alternative approaches to tether deployment and retrieval are discussed. It is shown that a relatively short tether system, 7 km long, operating at a power level of 5 kW could provide cumulative savings or over a billion dollars during a 10-year period ending in 2012. This savings is the direct result of a reduction in the number or nights that would otherwise be required to deliver propellant for reboost, with larger cost savings for higher tether usage. In addition to economic considerations, an electrodynamic tether promises a practical backup system that could ensure ISS survival in the event of an (otherwise) catastrophic delay in propellant delivery.
Document ID
20000032976
Acquisition Source
Marshall Space Flight Center
Document Type
Reprint (Version printed in journal)
Authors
Vas, Irwin E.
(Boeing Co. Huntsville, AL United States)
Kelly, Thomas J.
(Boeing Co. Huntsville, AL United States)
Scarl, Ethan A.
(Boeing Co. Huntsville, AL United States)
Date Acquired
September 7, 2013
Publication Date
November 1, 1999
Publication Information
Publication: Journal of Spacecraft and Rockets
Publisher: American Inst. of Aeronautics and Astronautics
Volume: 36
Issue: 6
Subject Category
Spacecraft Design, Testing And Performance
Funding Number(s)
CONTRACT_GRANT: NAS8-50000
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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