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Cure Cycle Design Methodology for Fabricating Reactive Resin Matrix Fiber Reinforced Composites: A Protocol for Producing Void-free Quality LaminatesFor the fabrication of resin matrix fiber reinforced composite laminates, a workable cure cycle (i.e., temperature and pressure profiles as a function of processing time) is needed and is critical for achieving void-free laminate consolidation. Design of such a cure cycle is not trivial, especially when dealing with reactive matrix resins. An empirical "trial and error" approach has been used as common practice in the composite industry. Such an approach is not only costly, but also ineffective at establishing the optimal processing conditions for a specific resin/fiber composite system. In this report, a rational "processing science" based approach is established, and a universal cure cycle design protocol is proposed. Following this protocol, a workable and optimal cure cycle can be readily and rationally designed for most reactive resin systems in a cost effective way. This design protocol has been validated through experimental studies of several reactive polyimide composites for a wide spectrum of usage that has been documented in the previous publications.
Document ID
20140012782
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Hou, Tan-Hung
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
October 2, 2014
Publication Date
September 1, 2014
Subject Category
Composite Materials
Report/Patent Number
NF1676L-19592
NASA/TM-2014-218524
L-20461
Report Number: NF1676L-19592
Report Number: NASA/TM-2014-218524
Report Number: L-20461
Funding Number(s)
WBS: WBS 544163.04.03.07.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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