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Systems analysis of electrodynamic tethersA dynamic simulation model is developed and employed in a new system study to investigate the performance of electrodynamic tethers, both as power generators and thrusters. The electron collection performance of a contactor and a bare wire tether, both separately and in combination, are compared and contrasted. The power and thrust generated by a bare wire tether is found to have a higher dependence on the geomagnetic and ionospheric fluctuations. However, depending on the performance of the contactor, the combination of a bare tether and contactor can substantially boost performance for power generation. As a pure thruster, the contactor tether is examined at constant current, voltage, thrust, and power. It is found that the best mode of operation is with constant power, with resulting power/thrust ratios better than those for ion or magnetoplasmadynamic engines. It is concluded that tethers offer greater potential than previously envisioned.
Document ID
19920058926
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Samantha Roy, R. I.
(NASA Lewis Research Center Cleveland, OH, United States)
Hastings, D. E.
(NASA Lewis Research Center Cleveland, OH, United States)
Ahedo, E.
(MIT Cambridge, MA, United States)
Date Acquired
August 15, 2013
Publication Date
June 1, 1992
Publication Information
Publication: Journal of Spacecraft and Rockets
Volume: 29
Issue: 3 Ma
ISSN: 0022-4650
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
ISSN: 0022-4650
Accession Number
92A41550
Funding Number(s)
CONTRACT_GRANT: NAG3-681
Distribution Limits
Public
Copyright
Other

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