No AccessMechanical Slosh Models for Rocket-Propelled SpacecraftsJiannwoei JangJiannwoei JangDraper LaboratorySearch for more papers by this authorAIAA 2013-4651Session: Spacecraft Dynamics Modeling and IdentificationPublished Online:15 Aug 2013https://doi.org/10.2514/6.2013-4651SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookXLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byAxisymmetric Ferrofluid Oscillations in a Cylindrical Tank in Microgravity23 July 2021 | Microgravity Science and Technology, Vol. 33, No. 4 What's Popular AIAA Guidance, Navigation, and Control (GNC) Conference August 19-22, 2013Boston, MAhttps://doi.org/10.2514/6.2013-4651 CrossmarkInformationCopyright © 2013 by The Charles Stark Draper Laboratory, Inc.. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. TopicsLiquid Rocket PropellantRocket PropellantRocketryRocketsSpace Systems and VehiclesSpace VehicleSpace Vehicle DesignSpacecrafts KeywordsSpacecraftsRocketsLiquid SloshingWeber NumberPropellantComputational Fluid DynamicsMATLABBernoulli's EquationBessel FunctionsAeronauticsDigital Topics Guidance, Navigation, and Control