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Thor-agena lateral bending vibration analysis final reportLateral bending vibration analysis for Thor- Agena test vehicle - rotary inertia, shear, and propellant sloshing
Document ID
19650024525
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Nowek, R. S.
(Douglas Aircraft Co., Inc. Santa Monica, CA, United States)
Stanton, E. L.
(Douglas Aircraft Co., Inc. Santa Monica, CA, United States)
Date Acquired
August 2, 2013
Publication Date
July 5, 1965
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-64971
SM-48944
Report Number: NASA-CR-64971
Report Number: SM-48944
Accession Number
65N34126
Funding Number(s)
CONTRACT_GRANT: NAS1-5156
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
VIBRATION EFFECT
THOR AGENA B LAUNCH VEHICLE
PROPELLANT
SLOSHING
SHEAR STRENGTH
LAUNCH VEHICLE
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