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Theory of plasma contactors for electrodynamic tethered satellite systemsRecent data from ground and space experiments indicate that plasma releases from an object dramatically reduce the sheath impedance between the object and the ambient plasma surrounding it. Available data is in qualitative accord with the theory developed to quantify the flow of current in the sheath. Electron transport in the theory is based on a fluid model of a collisionless plasma with an effective collision frequency comparable to frequencies of plasma oscillations. The theory leads to low effective impedances varying inversely with the square root of the injected plasma density. To support such a low impedance mode of operation using an argon plasma source, for example, requires that only one argon ion be injected for each thirty electrons extracted from the ambient plasma. The required plasma flow rates are quite low; to extract one ampere of electron current requires a mass flow rate of about one gram of argon per day.
Document ID
19870054335
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Parks, D. E.
(Systems Science and Software La Jolla, CA, United States)
Katz, I.
(Systems, Science and Software, La Jolla CA, United States)
Date Acquired
August 13, 2013
Publication Date
June 1, 1987
Publication Information
Publication: Journal of Spacecraft and Rockets
Volume: 24
ISSN: 0022-4650
Subject Category
Electronics And Electrical Engineering
Accession Number
87A41609
Funding Number(s)
CONTRACT_GRANT: NAS3-23881
Distribution Limits
Public
Copyright
Other

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