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Low-Earth Orbit Flight Test of an Inflatable Decelerator (LOFTID) Probabilistic Aeroshell Thermal Response Uncertainty Analysis
Document ID
20240000143
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Steven Tobin (Langley Research Center Hampton, United States)
Andrew Brune (Langley Research Center Hampton, United States)
Date Acquired
January 4, 2024
Subject Category
Spacecraft Design, Testing and Performance
Report/Patent Number
AIAA-2024-1499
Meeting Information
Meeting: AIAA SciTech Forum and Exposition
Location: Orlando, FL
Country: US
Start Date: January 8, 2024
End Date: January 12, 2024
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 833011.02.07.89UX.24
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
Single Expert

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