SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
Cornerstone Research Group, Inc.
2750 Indian Ripple Road
Dayton, OH 45440 - 3638
(937) 320-1877

PRINCIPAL INVESTIGATOR/PROJECT MANAGER (Name, E-mail, Mail Address, City/State/Zip, Phone)
Brian Henslee
hensleeb@crgrp.com
2750 Indian Ripple Rd
Dayton, OH 45440 - 3638
(937) 320-1877 Extension :1210

CORPORATE/BUSINESS OFFICIAL (Name, E-mail, Mail Address, City/State/Zip, Phone)
Chrysa Theodore
theodorecm@crgrp.com
2750 Indian Ripple Road
Dayton, OH 45440 - 3638
(937) 320-1877 Extension :1102

Estimated Technology Readiness Level (TRL) at beginning and end of contract:
Begin: 3
End: 5

Technology Available (TAV) Subtopics
In-Space Structural Assembly is a Technology Available (TAV) subtopic that includes NASA Intellectual Property (IP). Do you plan to use the NASA IP under the award?
No

TECHNICAL ABSTRACT (Limit 2000 characters, approximately 200 words)
CRG proposes to continue efforts from the 2016 NASA SBIR Phase I topic H5.04 Reclaimable Thermally Reversible Polymers for AM Feedstock. In Phase II, CRG will refine the thermally-reversible polymeric materials for function as reprocessable thermosetting matrixes, and evaluate improved reclamation and additive manufacturing (AM) related processing methods for prototype demonstrations. These materials and processes enable reclamation and repurposing of structural fiber-reinforced composites into new configurations during extraterrestrial missions, such as conversion to Additive Manufacturing (AM) feedstocks or direct fabrication into multipart constructs. The thermally-reversible thermosets also present the opportunity to generate volumes of AM feedstock through function as a binder matrix, allowing compounding and impregnation/infusion of in-situ resources such as environmentally sourced metallic, mineralogical (i.e. regolith), and desized/milled non-reprocessable composites. This approach will provide NASA with a means to support in-situ resource utilization with a reduced reliance on pristine raw material payloads. CRG has already demonstrated the efficacy of thermally-reversible polymer structures in commercial adhesive applications, as well as in previous NASA technical efforts for modifying waste packaging plastics to provide improved compatibility to AM processing (NASA SBIR H14.03-9603), and in the feasibility demonstration of the Phase I effort of this project. The proposed concept not only has the potential to enable resource reclamation and AM capability, but also to advance the state-of-the-art in AM materials technology. CRG's proposed approach to develop thermally-reversible polymer materials for thermoset polymer reprocessing, and demonstration of reclamation and manufacturing compatibility evaluation, will provide NASA with a material and processing technology readiness level (TRL) of 5 at the conclusion of the Phase II effort.

POTENTIAL NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
Supporting NASA's Human Exploration Destination Systems Technology Area and LaRC, this project's technologies directly address requirements for reducing launch mass by reclaiming launched structural components into recyclable manufacturing feedstock and providing polymeric technology for utilizing in-situ resources as composite AM raw materials. Recyclable composite materials would find potential in transport, colonization, habitat, and exploration systems. Future NASA space exploration and colonization missions will be planned to maximize available resources to enable mission success. Recyclable composites could play a significant role as an in-situ resource for those missions. This project's technologies offer the ability to manufacture components and structures on-site as needed through reclaiming structural composites that are no longer needed, allowing for reconfiguration of those same composites to new geometries, production of AM feedstock from the desized composites, and/or application of the reclaimable composite polymer matrix as a binder resin for larger volumes of environmental sourced particulate materials. This serves to reduce overall launch cost, and provides deep space exploration with additional tools to fabricate components and structures at mission destinations.

POTENTIAL NON-NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
This project's technologies, developed for NASA systems, would directly apply to systems operated by other government and commercial enterprises. Potential customers would be oriented toward emerging composite recycling markets and enhanced additive manufacturing feedstocks.
Example systems include rapid prototyping and additive manufacturing of complex, low-run number, and advanced design parts for systems operated by the Department of Defense. Prime defense contractors could find use of an enabling technology allowing 3-D printing of new and exotic polymeric materials or polymeric composites previously thought incompatible to additive manufacturing processes, including thermosetting systems.
This technology's attributes for improving the compatibility of polymers to AM systems would yield a high potential for private sector commercialization for AM and 3D printer manufactures, increasing the materials properties available in the feedstock. Companies could dramatically expand the properties of raw materials available to consumers, create new product lines based on thermosetting material designs, and potentially be able to produce materials with custom thermal-mechanical performance on-demand. The technology also enables businesses to additively manufacture components and systems previously impossible due to material limitations, and allows processes for the recycling and repair of composite materials previously incompatible to reuse after fabrication to first form.