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Jovian electrodynamic tether experimentA case is made for an electrodynamic tether scientific platform to be put into orbit around Jupiter as a follow-on to the present series of earth-based Tethered Satellite System (TSS) experiments. Preliminary system trades are made to bound the amount of power (assuming 100 percent plasma contactor efficiency) that can be obtained from the orbiting Jovian tether. With magnetic field strengths of roughly 4 to 7 Gauss, power levels of the order of 100 kilowatts can be obtained with a thin 500 km long tether. This should suffice to power a Jovian scientific experiment package. The electrodynamic tether also affords a loitering capability as it can be operated as a thruster in addition to a power generator. Further study and research is needed to characterize the Jovian tether as to its electrodynamic and dynamic performance potential. Hollow cathode plasma contactor operation needs to be verified in near earth space.
Document ID
19910036865
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hammond, Walter E.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Freeman, Scott E.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Nave, Mark J.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Rupp, Charles C.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1991
Subject Category
Astronautics (General)
Report/Patent Number
AIAA PAPER 91-0426
Report Number: AIAA PAPER 91-0426
Accession Number
91A21488
Distribution Limits
Public
Copyright
Other

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