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Solid Edge's Role and Modeling Techniques for Space Shuttle Flowliner Crack Investigation and Related ComponentsIn an effort to understand why the cracks were happening, the BTA was designed to measure the actual flow conditions surrounding the flowliners. A procedure was developed to fix the cracks by welding and polishing the affected smooth area.
Document ID
20040082370
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Goodman, Dwight D. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 21, 2013
Publication Date
January 1, 2004
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: Solid Edge Summit 2004
Location: Orlando, FL
Country: United States
Start Date: May 31, 2004
End Date: June 4, 2004
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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