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Composites Damage Tolerance WorkshopThe Composite Damage Tolerance Workshop included participants from NASA, academia, and private industry. The objectives of the workshop were to begin dialogue in order to establish a working group within the Agency, create awareness of damage tolerance requirements for Constellation, and discuss potential composite hardware for the Crew Launch Vehicle (CLV) Upper Stage (US) and Crew Module. It was proposed that a composites damage tolerance working group be created that acts within the framework of the existing NASA Fracture Control Methodology Panel. The working group charter would be to identify damage tolerance gaps and obstacles for implementation of composite structures into manned space flight systems and to develop strategies and recommendations to overcome these obstacles.
Document ID
20070002671
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Gregg, Wayne
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 24, 2013
Publication Date
January 1, 2006
Subject Category
Composite Materials
Meeting Information
Meeting: MSFC Damage Tolerance of Composites Workshop
Location: Huntsville, AL
Country: United States
Start Date: October 23, 2006
End Date: October 24, 2006
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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