Electrodynamic aspects of the first tethered satellite mission

Details Electrodynamic aspects of the first tethered satellite mission Electrodynamic aspects of the first tethered satellite mission

Aug 1993

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1993jgr....9813761d&link_type=abstract

Journal of Geophysical Research (ISSN 0148-0227), vol. 98, no. A8, p. 13,761-13,778.

Physics

Plasma Physics

32

Earth Ionosphere, Electrodynamics, Plasma Interactions, Space Plasmas, Tethered Satellites, Electric Fields, Magnetic Flux, Payloads, Spaceborne Experiments

Scientific paper

This paper aims at providing a thorough description of the basic electrodynamic aspects of a tethered satellite system (TSS) orbiting in the ionosphere. As will be seen, a wide variety of plasma physics phenomena are associated with the interaction of a conducting tether with the ionospheric plasma and, as a consequence, numerous basic science objectives can be addressed with a TSS system. Besides reviewing the various electrodynamic phenomena and our present knowledge on them, we provide also a description of the scientific payload and the nominal science objectives of the first tethered satellite project (TSS-1). A brief account, as well as a first evaluation, are also given of the mission itself, which was flown with the shuttle Atlantis launched on July 31, 1992.

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