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Electrodynamic tetherElectrodynamic tethers hold promise for a variety of space applications. Electrodynamic tethers depend upon the interactions between a moving insulated conductor and the Earth's magnetic field. An electric field is generated along the tether as in a conductor moving in the magnetic field of a generator. If the circuit is closed to the ambient space plasma via a plasma gun or other equivalent device, a current is enabled to flow in the tether, and electric power is generated at the expense of orbital mechanical energy. The net effect is a decrease in the altitude of the orbiting tethered system. The situation can be reversed by driving current against the electric field via an external power supply such as a photovoltaic array.
Document ID
19870017016
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Patterson, Michael
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
June 1, 1987
Publication Information
Publication: Space Photovoltaic Research and Technology 1986. High Efficiency, Space Environment and Array Technology
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
87N26449
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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