Stabilization of an injected conducting layer for artificially enhancing drag on orbital debris |
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| Authors: | R.B. Dahlburg L. Rudakov C. Crabtree G. Ganguli |
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| Affiliation: | 1. Laboratory for Computational Physics & Fluid Dynamics, Naval Research Laboratory, Washington, DC 20375, USA;2. Icarus Research Inc., P.O. Box 30780, Bethesda, MD 20824-0780, USA;3. Plasma Physics Division, Naval Research Laboratory, Washington, DC 20375, USA |
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| Abstract: | The evolution of a magnetized conducting medium suspended in magnetic and gravitational fields is examined. In this paper some effects of the influence of velocity fields on the linear stability properties of such layers are investigated. A fully compressible, three-dimensional analysis of the layer is described. The relevant equations are derived and then solved by the MagnetoHydroDynamic SPEctral Compressible Linear Stability (MHDSPECLS) algorithm, a Chebyshev collocation code. The code allows for the computation of magnetic and thermal effects. A complete stabilization of the system is found above a critical velocity of approximately 2500 m/s. |
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| Keywords: | Orbital debris Magnetohydrodynamics Numerical solution |
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