3D Printing of High Temperature Thermoset Foams for Space Vehicular Thermal Protection Systems
Contract Overview
Solicitation details, issuing organization, response deadlines, documents, and interested companies for this government contract opportunity.
AI Contract Overview
This NASA SBIR/STTR Phase II project, led by re:3D in collaboration with the University of Tennessee at Knoxville, focuses on developing a pilot system for the 3D printing and deposition of phenolic foam Thermal Protection Systems onto conformal, non-planar surfaces. The primary objective is to create a material extrusion system capable of applying a phenolic foam TPS surface to a scaled demonstration article, specifically an aluminum dome with a one-meter base diameter and radius of curvature. The technical scope includes the design and construction of a gantry printer based on the Terabot platform, featuring custom extruders with added degrees of motion, metering pumps for foam transport, in-situ defect monitoring, and advanced motion planning, followed by industrial curing and post-process machining. Parallel to the hardware development, research at the University of Tennessee will focus on refining foam material characteristics to reduce density and increase temperature stability. This includes exploring novel printing approaches to tailor elastic modulus and implementing graded compositions to enhance surface heat resistance, with validation conducted through plasma arc jet torch testing. This effort aims to replace expensive and labor-intensive manual layering processes with an automated additive manufacturing approach that allows for real-time component certification, the integration of sensors, and generative design based on engineering requirements. The project is designated as a total small business set-aside and is performed in Houston, Texas, and at the University of Tennessee.
General Info
Place of Performance
Houston, TX, 77058, USASet-Aside
Timeline
Organization & Contact Information
Interested Companies (2)
Full Description
Benefits: This process has applicability mission requiring an EDL phase dependent on parasitic surfaces for spacecraft survival. Current methods are expensive, labor intensive and result in non-optimum layering. In addition to cost benefits through material savings and automation, AM application of TPS surfaces offers real-time component certification, integration of sensors into the TPS during fabrication, & implementation of digital thread paradigms where TPS surfaces are generatively designed around engineering requirements. Outside of research institutions, to our knowledge there are no commercially available large-scale printers capable of applying thermoset foams to conformal, non-planar surfaces. With the resources of a Phase II grant, our collaboration with UTK, and partnerships with industry, we believe this project is achievable and will result in a process to industries beyond space and DoD customers.
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