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PAF Structural Test Design/AnalysisThe ET50 team was tasked with designing and analyzing various STE to support development and qualification tests for the Space Launch System (SLS) Payload Adapter Fitting (PAF). Axial, shear, and torsion load line assemblies are among the needed STE hardware. The product starts with a design concept with requirements by the customer.
Document ID
20240004574
Acquisition Source
Marshall Space Flight Center
Document Type
Poster
Authors
Hao Hua (Marshall Space Flight Center Redstone Arsenal, United States)
Ross Kreager (Marshall Space Flight Center Redstone Arsenal, United States)
Date Acquired
April 15, 2024
Subject Category
Structural Mechanics
Meeting Information
Meeting: Marshall Jamboree & Poster Expo
Location: Huntsville, AL
Country: US
Start Date: May 16, 2024
Sponsors: Marshall Space Flight Center
Funding Number(s)
WBS: 954879.01.01.62.99
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
Single Expert

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