NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Service tough composite structures using the Z-direction reinforcement processFoster-Miller has developed a new process to provide through thickness reinforcement of composite structures. The process reinforces laminates locally or globally on-tool during standard autoclave processing cycles. Initial test results indicate that the method has the potential to significantly reduce delamination in carbon-epoxy. Laminates reinforced with the z-fiber process have demonstrated significant improvements in mode 1 fracture toughness and compression strength after impact. Unlike alternative methods, in-plane properties are not adversely affected.
Document ID
19950021851
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Freitas, Glenn
(Foster-Miller Associates, Inc. Waltham, MA, United States)
Magee, Constance
(Foster-Miller Associates, Inc. Waltham, MA, United States)
Boyce, Joseph
(Foster-Miller Associates, Inc. Waltham, MA, United States)
Bott, Richard
(Naval Weapons Center China Lake, CA., United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1992
Publication Information
Publication: FAA, Ninth DOD(NASA)FAA Conference on Fibrous Composites in Structural Design, Volume 3
Subject Category
Composite Materials
Accession Number
95N28272
Funding Number(s)
CONTRACT_GRANT: N60530-88-C-0370
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available