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Electrodynamic interactionsPower and thrust applications of the electrodynamic tether are considered. The induced voltage in the tether wire is in the same direction in the case of a power generator and a spacecraft motor, and the difference involves whether one allows that voltage to drive a current to generate power. Or, if one uses an onboard power supply with a higher voltage to drive a current in the opposite direction, which then provides thrust. Return circuit currents must be spread out through the ionosphere sufficiently so that ionosphere conductivities are very high and so that anomalous resistance is not produced in the ionosphere which would prevent the current from flowing. This is largely a function of the plasma contactors that are used. Three have been most frequently considered. It is concluded that, for the primary power and thrust applications, the hollow cathode seems to be far superior to the electron gun for producing high current contact to the ionosphere. This has led to a study of the Plasma Motor Generator (PMG) because it is capable of being reversed. The PMG theory is explored along with other power and thrust applications of the electrodynamic tether.
Document ID
19860018943
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mccoy, J.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
August 12, 2013
Publication Date
June 1, 1986
Publication Information
Publication: NASA, Washington Applications of Tethers in Space: Workshop Proceedings, Volume 1
Subject Category
Astronautics (General)
Accession Number
86N28415
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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