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On the use of magnetohydrodynamics during high speed re-entryMagnetic field interaction with hypersonic flow to effect deceleration and heating during reentry
Document ID
19650010875
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Jarvinen, P. O.
Date Acquired
August 2, 2013
Publication Date
April 1, 1965
Subject Category
Physics, Plasma
Report/Patent Number
NASA-CR-206
Report Number: NASA-CR-206
Accession Number
65N20476
Funding Number(s)
CONTRACT_GRANT: NASW-748
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
HYPERSONIC FLOW
DECELERATION
MAGNETIC FIELD
REENTRY
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