Search NASA⌕ Search

NASA NTRS · 20190000477

Polymer Matrix Composites Fabrication and Testing

Abstract

This 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.

Keep this discovery

Explore connections, maps & timelines

BibTeXRIS

Miller, Sandi, Conradi, Chris, Devine, Ryan, Heimann, Paula. 2018-08-02. Polymer Matrix Composites Fabrication and Testing. https://ntrs.nasa.gov/citations/20190000477

Cite the original work for its findings. Save a collection to share your selection of sources.