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Kinetic performance of barrier-cooled rocket nozzles.Flow of chemically reacting propellant exhaust mixture in barrier cooled axisymmetric rocket nozzle
Document ID
19680062125
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Frey, H. M.
Kliegel, J. R.
Melde, J. E.
Nickerson, G. R.
Quan, V.
Date Acquired
August 4, 2013
Publication Date
October 1, 1968
Subject Category
Aerodynamics
Accession Number
68A43097
Funding Number(s)
CONTRACT_GRANT: NAS9-4358
Distribution Limits
Public
Copyright
Other

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