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Propellant slosh coupling with bending Final reportFlight simulation model for combined bending and slosh modes of Saturn 5 launch vehicles
Document ID
19700011112
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Feng, G. C.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Grady, D. L.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Date Acquired
September 2, 2013
Publication Date
December 1, 1969
Subject Category
Space Vehicles
Report/Patent Number
NASA-CR-102487
LMSC/HREC-D149410
HREC-1485-2
Report Number: NASA-CR-102487
Report Number: LMSC/HREC-D149410
Report Number: HREC-1485-2
Accession Number
70N20417
Funding Number(s)
CONTRACT_GRANT: NAS8-21485
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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