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Damage Tolerance of Composites (2007)

Hodge, Andy

In: CASI

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Publication Date: 2019-07-13

Description: Fracture 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.

Keywords: Composite Materials

Type: National Space and Missile Materials Symposium; Jun 25, 2007 - Jun 29, 2007; Keystone, CO; United States

Format: application/pdf

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