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Validation of Slosh Model Parameters and Anti-Slosh Baffle Designs of Propellant Tanks by Using Lateral Slosh TestingThe slosh dynamics of propellant tanks can be represented by an equivalent mass-pendulum-dashpot mechanical model. The parameters of this equivalent model, identified as slosh mechanical model parameters, are slosh frequency, slosh mass, and pendulum hinge point location. They can be obtained by both analysis and testing for discrete fill levels. Anti-slosh baffles are usually needed in propellant tanks to control the movement of the fluid inside the tank. Lateral slosh testing, involving both random excitation testing and free-decay testing, are performed to validate the slosh mechanical model parameters and the damping added to the fluid by the anti-slosh baffles. Traditional modal analysis procedures were used to extract the parameters from the experimental data. Test setup of sub-scale tanks will be described. A comparison between experimental results and analysis will be presented.
Document ID
20130000590
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Perez, Jose G.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Parks, Russel, A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Lazor, Daniel R.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 27, 2013
Publication Date
October 16, 2012
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
M12-1999
Meeting Information
Meeting: 28th Aerospace Testing Seminar
Location: Los Angeles, CA
Country: United States
Start Date: October 16, 2012
End Date: October 18, 2012
Sponsors: Aerospace Corp., Jet Propulsion Lab., California Inst. of Tech.
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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