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Comparison of propellant sloshing parameters obtained from model and full-size Centaur liquid-oxygen tanksComparison of propellant sloshing and pendulum analogy parameters from Centaur liquid-oxygen tanks
Document ID
19660027849
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Stofan, A. J. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
September 1, 1966
Subject Category
Propellants
Report/Patent Number
NASA-TM-X-1286
Report Number: NASA-TM-X-1286
Accession Number
66N37139
Funding Number(s)
CONTRACT_GRANT: 891-01-00-06-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LIQUID OXYGEN /LOX/
CENTAUR LAUNCH VEHICLE
LIQUID SLOSHING
PROPELLANT TANK

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