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Propellant vibrations in rocket tanks and their effect upon overall stability Effect of propellant sloshing upon stability of rocket having simple coordinate system with accelerometer
Document ID
19640037174
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Bauer, H. F.
Date Acquired
August 2, 2013
Publication Date
June 1, 1964
Subject Category
Space Vehicles
Accession Number
64A23067
Distribution Limits
Public
Copyright
Other
Keywords
LIQUID SLOSHING
PROPELLANT TANK

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