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Polymer Matrix Composites Fabrication and TestingThis project involves two separate processes for fabricating carbon fiber composite parts using Hexcel’s RTM6 resin system and Kaneka’s IR-6070 toughened resin system to impregnate carbon fiber tow and weave. These two resins were chosen to model microcracking in parts using RTM6 compared to parts using IR-6070. Plies of the composites were made by painting resin onto 8 harness satin weave or impregnating IM7 12k tow in a prepregging machine. Plies were consolidated using an out-of-autoclave oven or a heat press. Fabrication of the composite parts were conducted with the end goal of sending the composites to be tested and modeled for microcracking. The data will be used for computer modeling in the future.
Document ID
20190000477
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Miller, Sandi
(NASA Glenn Research Center Cleveland, OH, United States)
Conradi, Chris
(Louisiana Univ. Lafayette, LA, United States)
Devine, Ryan
(University School Hunting Valley, OH, United States)
Heimann, Paula
(Ohio Aerospace Inst. Cleveland, OH, United States)
Date Acquired
February 9, 2019
Publication Date
August 2, 2018
Subject Category
Composite Materials
Report/Patent Number
GRC-E-DAA-TN59122
Report Number: GRC-E-DAA-TN59122
Meeting Information
Meeting: Annual Northeast Ohio Undergraduate Research Symposium (NOURS)
Location: Kent, OH
Country: United States
Start Date: August 2, 2018
Sponsors: Cleveland State Univ.
Funding Number(s)
WBS: WBS 585777.04.70.30.22
CONTRACT_GRANT: NNC13BA10B
CONTRACT_GRANT: NNC16QA09D
Distribution Limits
Public
Copyright
Public Use Permitted.
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