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Electrodynamic Tether Operations beyond the Ionosphere in the Low-Density MagnetosphereIn the classical concept for the operation of electrodynamic tethers in space, a voltage is generated across the tether, either by the tether's orbital motion through the earth's planetary magnetic field or by a power supply; electrons are then collected from the ionospheric plasma at the positive pole; actively emitted back into space at the negative pole; and the circuit is closed by currents driven through the ambient conducting ionosphere. This concept has been proven to work in space by the Tethered Satellite System TSS-1 and TSS-1R Space Shuttle missions; and the Plasma Motor-Generator (PMG) tether flight experiment. However, it limits electrodynamic tether operations to the F-region of the ionosphere where the plasma density is sufficient to conduct the required currents--in other words, between altitudes of approximately 200 to 1000 km in sunlight. In the earth's shadow, the ionospheric density drops precipitously and tether operations, using the above approach, are not effective--even within this altitude range. There are numerous missions that require in-space propulsion in the Earth's shadow and/or outside of the above altitude range. This paper will, therefore, present the fundamentals of a concept that would allow electrodynamic tethers to operate almost anywhere within the magnetosphere, the region of space containing the earth's planetary magnetic field. In other words, because operations would be virtually independent of any ambient plasma, the range of electrodynamic operations would be extended into the earth's shadow and out to synchronous orbit--forty times the present operational range. The key to this concept is the active generation of plasma at each pole of the tether so that current generation ,does not depend on the conductivity of the ambient ionosphere. Arguments will be presented, based on ,existing flight data, which shed light on the behavior of charge emissions in space and show the plausibility of the concept.
Document ID
20070031721
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Stone, Nobie H.
(Spectra Research Systems, Inc. Huntsville, AL, United States)
Date Acquired
August 23, 2013
Publication Date
May 14, 2007
Subject Category
Plasma Physics
Meeting Information
Meeting: 54th JANNAF Propulsion Meeting/5th Modeling and Simulation/3rd Liquid Propulsion/2nd Spacecraft Propulsion Joint Subcommittee
Location: Denver, CO
Country: United States
Start Date: May 14, 2007
End Date: May 17, 2007
Sponsors: Department of the Army, Department of the Air Force, NASA Headquarters, Department of the Navy
Funding Number(s)
CONTRACT_GRANT: NNM04AA11C
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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