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Electrodynamic tetherThe electrodynamic tether consists of a satellite deployed to a distance of 20 km by an electrically conducting tether. The space station hardware consists of a 12 meter deployment boom, satellite cradle, tether reel and motor, and other tether support systems. The electrodynamic tether will be used to perform a variety of wave experiments by exciting a wide spectrum of low frequency waves in the ionospheric plasma. The system can also be used to artificially generate and study field aligned currents and associated plasma effects. Hydromagnetic waves generated by the passage of the system through the space plasma are of particular interest in space plasma research.
Document ID
19850025855
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Roberts, W. T.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1985
Publication Information
Publication: Alabama Univ. Coordinated Study of Solar-Terrestrial Payloads on Space Station
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
85N34168
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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