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Studies on ionization phenomena associated with solid propellant rockets.Solid propellant composition and rocket motor design effect on plasma microwave and visible light attenuation emitted by exhaust
Document ID
19650031904
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Capener, E. L.
Chown, J.
Dickinson, L. A.
Nanevicz, J. E.
Date Acquired
August 2, 2013
Publication Date
February 1, 1965
Subject Category
Communications
Report/Patent Number
AIAA PAPER 65-182
Report Number: AIAA PAPER 65-182
Accession Number
65A14608
Funding Number(s)
CONTRACT_GRANT: NAS7-179
Distribution Limits
Public
Copyright
Other
Keywords
COMPOSITE PROPELLANT
ROCKET EXHAUST
SOLID PROPELLANT ROCKET ENGINE
LIGHT TRANSMISSION
MICROWAVE ATTENUATION

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