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Backshell Thermal Protection Materials for Additive ManufacturingLeveraging AM technology focused on the Fused Deposition Modeling (FDM) process could automate the heat shield manufacturing process and allow it to reduce cost and build time and improve the design to 3D print and process TPS materials directly on the structure in monolith segments. Furthermore, AM allows the production of complicated three-dimensional geometry and density gradient layers without custom molds or special tools. NASA invests in additive manufacturing (AM) to enable new mission architectures and design methods; AM is suited for backshell thermal protection materials that require many complex closeouts that lead to integration challenges. Current work will review backshell thermal protection material formulation, development, and characterization.3D printer was used to 3D print arc-jet test coupons. The coupons were tested at the NASA Ames arc jet facility, and the results show promising properties compared with the heritage materials.
Document ID
20210026622
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Tane Boghozian
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Gurpreet Klar
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Adam Thomas Sidor
(Johnson Space Center Houston, Texas, United States)
Stanley A Bouslog
(Johnson Space Center Houston, Texas, United States)
Date Acquired
January 11, 2022
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: The NSMMS & CRASTE Joint Symposia
Location: TBD
Country: US
Start Date: June 27, 2022
End Date: June 30, 2022
Sponsors: Commercial and Government Responsive Access to Space Technology Exchange, National Space & Missile Materials Symposium
Funding Number(s)
PROJECT: ECI project
CONTRACT_GRANT: NNA15BB15C
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Technical Management
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