Deployment of a long-tethered connection between two bodies in orbit

Details Deployment of a long-tethered connection between two bodies in orbit Deployment of a long-tethered connection between two bodies in orbit

Jan 1983

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1983kosis..21..121l&link_type=abstract

Kosmicheskie Issledovaniia, vol. 21, Jan.-Feb. 1983, p. 121-124. In Russian.

Physics

Elliptical Orbits, Geosynchronous Orbits, Orbit Perturbation, Tethered Satellites, Deployment, Drift Rate, Structural Vibration

Scientific paper

A sufficiently simple method is described for the deployment of a long-tethered satellite system in elliptical orbit. A class of motions of a variable-length tether is examined. Equations are derived for describing horizontal oscillations of the probe (the tethered body) near the vertical-drift regime in the orbit plane and for oscillations in the direction of the normal to the orbit plane.

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