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Fracture Control Requirements for Composite and Bonded StructuresCurrent new requirements document are top level or specific to shuttle payloads. NASA-STD-5007 top level requirement that imposes fracture control on all manned spacecraft hardware. Composites addressed at very top level. NASA_SDT-5003 imposes fracture control on payloads for the space shuttle. Imposes fracture control on composite and bonded structures. Silent on many important issues such as post proof NDE, residual strength, and reuse. Not adequate for or directly applicable to next generation of spacecraft.
Document ID
20040084077
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Faile, Gwyn C. (Qualis Corp. Huntsville, AL, United States)
Date Acquired
August 21, 2013
Publication Date
January 1, 2004
Subject Category
Documentation And Information Science
Report/Patent Number
MG-04-0205
Report Number: MG-04-0205
Meeting Information
Meeting: NASA Fracture Control Methodology Panel
Location: San Antonio, TX
Country: United States
Start Date: June 2, 2004
End Date: June 4, 2004
Funding Number(s)
OTHER: 794-40-4C
Distribution Limits
Public
Copyright
Public Use Permitted.

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