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STABILITY BOUNDARIES OF LIQUID-PROPELLED SPACE VEHICLES WITH SLOSHINGStability boundaries of space vehicles due to liquid propellant sloshing, sloshing mass, sloshing frequency, and tank location
Document ID
19630023364
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Bauer, H. F.
Date Acquired
August 1, 2013
Publication Date
July 1, 1963
Subject Category
Space Sciences
Accession Number
63A19423
Distribution Limits
Public
Copyright
Other
Keywords
LIQUID SLOSHING
PROPELLANT TANK
SPACECRAFT STABILITY
MISSILE STABILIZATION
SLOSHING
ROCKET FUEL TANK

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