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Damage tolerance of composites
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Hodge, Andy |
| Copyright Year | 2007 |
| 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. |
| File Size | 1523257 |
| Page Count | 32 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20070031963 |
| Archival Resource Key | ark:/13960/t59d1x70s |
| Language | English |
| Publisher Date | 2007-06-25 |
| Access Restriction | Open |
| Subject Keyword | Composite Materials Nondestructive Tests Damage Assessment Handbooks Durability Manned Space Flight Defense Program Impact Damage Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
