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Towards the Prediction of Entry Capsule Dynamic Stability Characteristics with Reduced Free Flight Motion in FUN3DWork is done to verify FUN3D's 6-DOF path and begin active application to flight projects. This work moves towards a computational predictive capability for entry capsule dynamic stability such that data from concurrent ground testing will enable validation efforts of this solver and its continued use on EDL vehicles. Applications of the solver to the Dragonfly mission to Titan and the Mars Sample Return - Earth Entry System are discussed.
Document ID
20220012339
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Eli Shellabarger (Langley Research Center Hampton, Virginia, United States)
Date Acquired
August 9, 2022
Subject Category
Spacecraft Design, Testing And Performance
Computer Programming And Software
Meeting Information
Meeting: Thermal and Fluids Analysis Workshop (TFAWS)
Location: Virtual
Country: US
Start Date: September 6, 2022
End Date: September 9, 2022
Sponsors: National Aeronautics and Space Administration
Funding Number(s)
WBS: 869021.05.23.05.46
WBS: 829688.14.02.06
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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