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Modeling and Simulation Techniques for the NASA SLS Service Module Panel Separation Event; from Loosely-Coupled Euler to Fully-Coupled 6-DOF, Time-Accurate, Navier-Stokes MethodologiesNo abstract available
Document ID
20190000732
Acquisition Source
Marshall Space Flight Center
Document Type
Presentation
Authors
Hall, Les H. (Jacobs Engineering Group, Inc. Huntsville, AL, United States)
Date Acquired
February 14, 2019
Publication Date
January 7, 2019
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
M18-7140
Meeting Information
Meeting: AIAA Science and Technology (SciTech) Forum
Location: San Diego, CA
Country: United States
Start Date: January 7, 2019
End Date: January 11, 2019
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.

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