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Use of Higher Fidelity Slosh Models to Reduce Conservatism in Launch Vehicle Flight Control DesignsNo abstract available
Document ID
20150021445
Acquisition Source
Marshall Space Flight Center
Document Type
Presentation
Authors
Hall, Robert A. (Jacobs Engineering and Science Services and Skills Augmentation Group (ESSSA) Huntsville, AL, United States)
Date Acquired
November 19, 2015
Publication Date
October 2, 2015
Subject Category
Propellants And Fuels
Spacecraft Design, Testing And Performance
Report/Patent Number
M16-4921
Report Number: M16-4921
Funding Number(s)
CONTRACT_GRANT: NNM12AA41C
Distribution Limits
Public
Copyright
Public Use Permitted.

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