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Electrodynamic Tether Propulsion and Power Generation at JupiterThe results of a study performed to evaluate the feasibility and merits of using an electrodynamic tether for propulsion and power generation for a spacecraft in the Jovian system are presented. The environment of the Jovian system has properties which are particularly favorable for utilization of an electrodynamic tether. Specifically, the planet has a strong magnetic field and the mass of the planet dictates high orbital velocities which, when combined with the planet's rapid rotation rate, can produce very large relative velocities between the magnetic field and the spacecraft. In a circular orbit close to the planet, tether propulsive forces are found to be as high as 50 N and power levels as high as 1 MW.
Document ID
19980203952
Document Type
Technical Publication (TP)
Authors
Gallagher, D. L. (NASA Marshall Space Flight Center Huntsville, AL United States)
Johnson, L. (NASA Marshall Space Flight Center Huntsville, AL United States)
Moore, J. (Spectra Research Systems, Inc. Huntsville, AL United States)
Bagenal, F. (Colorado Univ. Boulder, CO United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1998
Subject Category
Spacecraft Propulsion and Power
Report/Patent Number
NAS 1.60:208475
M-876
NASA/TP-1998-208475
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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