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Experimental, Numerical and Analytical Characterization of Slosh Dynamics Applied to In-Space Propellant Storage, Management and TransferExperimental and numerical results are presented from a new cryogenic fluid slosh program at the Florida Institute of Technology (FIT). Water and cryogenic liquid nitrogen are used in various ground-based tests with an approximately 30 cm diameter spherical tank to characterize damping, slosh mode frequencies, and slosh forces. The experimental results are compared to a computational fluid dynamics (CFD) model for validation. An analytical model is constructed from prior work for comparison. Good agreement is seen between experimental, numerical, and analytical results.
Document ID
20150018438
Acquisition Source
Kennedy Space Center
Document Type
Presentation
Authors
Storey, Jed
(Florida Inst. of Tech. Melbourne, FL, United States)
Lapilli, Gabriel D.
(Florida Inst. of Tech. Melbourne, FL, United States)
Kirk, Daniel
(Florida Inst. of Tech. Melbourne, FL, United States)
Gutierrez, Hector
(Florida Inst. of Tech. Melbourne, FL, United States)
Marsell, Brandon
(NASA Kennedy Space Center Cocoa Beach, FL United States)
Schallhorn, Paul
(NASA Kennedy Space Center Cocoa Beach, FL United States)
Date Acquired
September 28, 2015
Publication Date
July 27, 2015
Subject Category
Spacecraft Design, Testing And Performance
Propellants And Fuels
Report/Patent Number
KSC-E-DAA-TN25160
Meeting Information
Meeting: AIAA/SAE/ASEE Joint Propulsion Conference
Location: Orlando, FL
Country: United States
Start Date: July 27, 2015
End Date: July 29, 2015
Sponsors: American Inst. of Aeronautics and Astronautics, American Society for Electrical Engineers, Society of Automotive Engineers, Inc.
Funding Number(s)
CONTRACT_GRANT: NNX14AM08H
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
slosh
cryogenics
slosh mode frequencies
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