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Studies on ionization phenomena associated with solid-propellant rockets.Microwave attenuation magnitude associated with exhaust plasma of nonaluminized and aluminized composite propellant
Document ID
19660059397
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Capener, E. L.
Chown, J. B.
Dickinson, L. A.
Nanevicz, J. E.
Date Acquired
August 3, 2013
Publication Date
August 1, 1966
Publication Information
Publication: /AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Subject Category
Propulsion Systems
Accession Number
66A38687
Funding Number(s)
CONTRACT_GRANT: NAS7-179
Distribution Limits
Public
Copyright
Other
Keywords
COMPOSITE PROPELLANT
MICROWAVE ATTENUATION
ROCKET EXHAUST
EXHAUST JET
SOLID PROPELLANT ROCKET ENGINE

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