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Damage Tolerance of CompositesFracture control requirements have been developed to address damage tolerance of composites for manned space flight hardware. The requirements provide the framework for critical and noncritical hardware assessment and testing. The need for damage threat assessments, impact damage protection plans, and nondestructive evaluation are also addressed. Hardware intended to be damage tolerant have extensive coupon, sub-element, and full-scale testing requirements in-line with the Building Block Approach concept from the MIL-HDBK-17, Department of Defense Composite Materials Handbook.
Document ID
20070031963
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Hodge, Andy
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 23, 2013
Publication Date
June 25, 2007
Subject Category
Composite Materials
Meeting Information
Meeting: National Space and Missile Materials Symposium
Location: Keystone, CO
Country: United States
Start Date: June 25, 2007
End Date: June 29, 2007
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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