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Superconducting applications in propulsion systems. Magnetic insulation for plasma propulsion devicesThe 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.
Document ID
19930002825
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Gonzalez, Dora E.
(Alabama Univ. Huntsville, AL, United States)
Karr, Gerald R.
(Alabama Univ. Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1990
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-CR-184401
NAS 1.26:184401
Report Number: NASA-CR-184401
Report Number: NAS 1.26:184401
Accession Number
93N12013
Funding Number(s)
CONTRACT_GRANT: NAS8-36955
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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