GEOCOMPOSITES, LLC, AIMS TO DEVELOP THE NEXT GENERATION OF HIGH PERFORMANCE FIBER REINFORCED COMPOSITE FEED…

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GEOCOMPOSITES, LLC, AIMS TO DEVELOP THE NEXT GENERATION OF HIGH PERFORMANCE FIBER REINFORCED COMPOSITE FEEDSTOCK FOR IN-SPACE MANUFACTURING OF HIGH STRENGTH PARTS VIA FUSED DEPOSITION MODELING (FDM). SINCE PLASTICS ARE INHERENTLY LOW IN STRENGTH, ADDITIVE MANUFACTURED PLASTIC CURRENTLY CANNOT COMPETE WITH METALLIC PARTS. FAILED PARTS ON THE INTERNATIONAL SPACE STATION (ISS) AND THE GENUINE NEED FOR STRUCTURAL SPARE PARTS ONBOARD ISS AND FOR DEEP SPACE MISSIONS MANDATES THAT COMPOSITE FEEDSTOCK AND ASSOCIATED FDM PAYLOADS SHOULD BE DEVELOPED FOR FUTURE IN-SPACE MANUFACTURING. GEOCOMPOSITES WILL DEVELOP COMPOSITE FEEDSTOCKS AND ASSOCIATED DEPOSITION PARAMETERS TO MEET THE REQUIREMENT SET BY NASA FOR AN ULTIMATE TENSILE STRENGTH OF 200 MPA. FOR A HIGH STRENGTH PART, IT IS NOT JUST SUFFICIENT TO HAVE A HIGH STRENGTH FEEDSTOCK BUT ALSO A FDM FACILITY THAT ALLOWS FOR THE PART BUILD AS DICTATED BY THE FEEDSTOCK. GEOCOMPOSITES PROPOSES TO DEMONSTRATE A COMBINATION OF FEEDSTOCKS FOR HIGH STRENGTH PARTS. THE PART BUILD WILL BE PERFORMED WITH A DUAL NOZZLE FDM MACHINE. THE FIRST FEEDSTOCK WILL BE CREATED BY EXTRUDING THE MIXTURE OF A THERMOPLASTIC MATRIX WITH AN OPTIMIZED DISTRIBUTION OF COMPATIBLE CHOPPED FIBERS. CONTINUITY BETWEEN THE INTERLAYER FIBERS WILL PROVIDE HIGH BOND STRENGTH BETWEEN LAYERS. THE LAYUP WILL COMBINE THIS FEEDSTOCK WITH CONTINUOUS HIGH STRENGTH HIGH TEMPERATURE (HSHT) FIBERS. MECHANICAL AND OUTGAS TESTING WILL BE PERFORMED TO DEMONSTRATE COMPATIBILITY WITH NASA REQUIREMENTS. IN ADDITION, WE PROPOSE TO ANALYZE ISS ACCOMMODATION OF FDM EQUIPMENT CAPABLE OF PRINTING STRUCTURAL PARTS ON THE ISS USING THE DEVELOPED FEEDSTOCKS. THE OVERALL PROPOSED APPROACH WILL PROVIDE A COMPREHENSIVE SOLUTION TO INCLUDE DEVELOPMENT OF THE CUSTOMIZED HIGH STRENGTH FEEDSTOCKS, LAYUP PATTERN AND BUILD PARAMETERS, AND AN ANALYSIS OF ISS ACCOMMODATION FOR CONSISTENT INSPACE PRODUCTION OF HIGH STRENGTH COMPOSITE PARTS.