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A Fluid-Structure Interaction Study of Re-entry Vehicles with Inflatable Decelerators and Validation of Methodologies against Wind Tunnel Test Data, Past, and Future
Document ID
20200005556
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Sasan Armand
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
May 13, 2020
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NF1676L-12877
Meeting Information
Meeting: Spacecraft and Launch Vehicle Dynamic Environment Workshop
Location: El Segundo, CA
Country: US
Start Date: June 4, 2019
End Date: June 6, 2019
Sponsors: Aerospace Corp.
Funding Number(s)
WBS: 644423.10.36.02.04.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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