The purpose of this paper is to review the status of knowledge of the basic concepts needed to establish design parameters for effective magnetic insulation. The objective is to estimate the effectiveness of the magnetic field in insulating the plasma, to calculate the magnitude of the magnetic field necessary to reduce the heat transfer to the walls sufficiently enough to demonstrate the potential of magnetically driven plasma rockets.
Superconducting applications in propulsion systems. Magnetic insulation for plasma propulsion devices
01.06.1990
Report
Keine Angabe
Englisch
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