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Propulsion From a Rotating EM Tether at JupiterThe Jovian system with its rapid planetary rotation and strong magnetic field presents exciting opportunities for the use of electrodynamic (EM) tethers. Previous analysis for a radial, 10 km length tether demonstrated the possibility of propulsive forces as large as 50 Newtons near the planet. For orbital positions beyond about 2.5 Jovian radii, an EM tether can simultaneously be used for power and increases in the orbital altitude. Although the previous study demonstrated the physical feasibility of EM tether use at Jupiter, it did not address the issues of limited gravity gradient force for tether orientation and the practical use of this technology in an engineered system. This presentation will discuss these issues and current progress in an ongoing science/engineering transitional study.
Document ID
20000021509
Acquisition Source
Marshall Space Flight Center
Document Type
Abstract
Authors
Gallagher, D. L.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Moore, J.
(SRS Technologies Huntsville, AL United States)
Date Acquired
August 19, 2013
Publication Date
January 1, 2000
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: Aerospace Science
Location: Reno, NV
Country: United States
Start Date: January 10, 2000
End Date: January 13, 2000
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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