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Nonlinear Propellant Slosh Damping Testing, Analysis, and Implementation for Launch Vehicle Flight Controls
Part 1: Testing, Analysis and Model Development
Document ID
20220013819
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Tannen VanZwieten
(Kennedy Space Center Merritt Island, Florida, United States)
Date Acquired
September 9, 2022
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: NASA/ESA Interagency G&C Seminar Series
Location: Virtual
Country: US
Start Date: September 15, 2022
Sponsors: European Space Agency, National Aeronautics and Space Administration
Funding Number(s)
WBS: 869021.01.23.01.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
Single Expert
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