NASA SBIR 2018-I Solicitation

Proposal Summary


PROPOSAL NUMBER:
 18-1- H7.01-9532
SUBTOPIC TITLE:
 Development of Higher Strength Feedstocks for In-Space Manufacturing
PROPOSAL TITLE:
 Development of Fiber Reinforced Composite Feedstock for In-Space Manufacturing of High Strength Parts
SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
GeoComposites, LLC
111 Veterans Memorial Boulevard, Suite 1600
Metairie , LA 70005-3044
(504) 405-3386

Principal Investigator (Name, E-mail, Mail Address, City/State/Zip, Phone)
Dr. Sunil Patankar
Sunil.patankar@geocent.com
111 Veterans Memorial Blvd., Suite 1600 Metairie, LA 70005 - 3044
(256) 489-4748

Business Official (Name, E-mail, Mail Address, City/State/Zip, Phone)
Mr. Jeff Tomeny
GeoComposites@geocent.com
111 Veterans Memorial Blvd., Suite 1600 Metairie, LA 70005 - 3044
(504) 831-1900
Estimated Technology Readiness Level (TRL) :
Begin: 2
End: 4
Technical Abstract

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 in-space production of high strength composite parts.

Potential NASA Applications

High strength feedstocks and an ISS-compatible FDM machine will provide the path for:

· In-space manufacturing of structures, electronics, and tools;

· Printed satellites, including CubeSats;

· Mass savings on Space Launch Systems by replacing metallic parts with composites;

· Printing of multifunctional radiation shielding material for crew health;

· In-space part design using digital twins validated by real time diagnostics;

· On-demand printing of food using cellulose based feedstocks.

Potential Non-NASA Applications

Non-NASA applications of FDM using high strength feedstock is expected to include:

· For the medical industry, products ranging from medical devices to cell culturing;

· For the aerospace industry, items like GE’s commercial jet engine nozzle;

· For construction, fiber reinforced building material feedstock and Contour Crafting;

· For the automotive industry, lightweight printed composites to enhance fuel efficiency;

· For the Department of Defense, on demand printed parts in theater of operation.


Form Generated on 05/25/2018 11:30:01