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Europa Clipper Preliminary Design Review Propellant Slosh AnalysisPropellant slosh was analyzed for both the oxidizer and the fuel for the Europa Clipper propulsion system. Slosh was examined for various fill fractions for cases where acceleration was on the order of magnitude of 10(exp -2) m/sq. s using the computational fluid dynamics software package STAR-CCM+ and at various fill fractions for cases where acceleration was on the order of magnitude of 10(exp -5) m/sq. s using Surface Evolver. Equivalent mechanical model parameters were derived from the CFD data using MATLAB for both the higher and the lower acceleration slosh cases. These parameters were plotted and can be used to interpolate mechanical model parameters at fill fractions not analyzed by CFD or Surface Evolver.
Document ID
20180004495
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Beckman, Emily A.
Benson, David J.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Cataldo, Daniel J.
(SGT, Inc. Greenbelt, MD, United States)
Ng, Wanyi W.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 16, 2018
Publication Date
July 9, 2018
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
GSFC-E-DAA-TN57194
Report Number: GSFC-E-DAA-TN57194
Meeting Information
Meeting: AIAA/SAE/ASEE Joint Propulsion Conference
Location: Cincinnati, OH
Country: United States
Start Date: July 9, 2017
End Date: July 11, 2017
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNJ14RA01B
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Keywords
CFD
Surface Evolver
slosh
propellant tank
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