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Development of 3D Woven Ablative Thermal Protection Systems (TPS) for NASA SpacecraftThe development of a new class of thermal protection system (TPS) materials known as 3D Woven TPS led by the Entry Systems and Technology Division of NASA Ames Research Center (ARC) will be discussed. This effort utilizes 3D weaving and resin infusion technologies to produce heat shield materials that are engineered and optimized for specific missions and requirements. A wide range of architectures and compositions have been produced and preliminarily tested to prove the viability and tailorability of the 3D weaving approach to TPS.
Document ID
20150022378
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
Feldman, Jay D.
(Analytical Mechanics Associates, Inc. Mountain View, CA, United States)
Ellerby, Don
(NASA Ames Research Center Moffett Field, CA, United States)
Stackpoole, Mairead
(NASA Ames Research Center Moffett Field, CA, United States)
Peterson, Keith
(Analytical Mechanics Associates, Inc. Mountain View, CA, United States)
Venkatapathy, Ethiraj
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
December 8, 2015
Publication Date
October 30, 2015
Subject Category
Spacecraft Design, Testing And Performance
Fluid Mechanics And Thermodynamics
Report/Patent Number
ARC-E-DAA-TN27338
Report Number: ARC-E-DAA-TN27338
Meeting Information
Meeting: South Texas Society for the Advancement of Materials and Process Engineering (SAMPE) Chapter Meeting
Location: Austin, TX
Country: United States
Start Date: October 30, 2015
Sponsors: Society for the Advancement of Materials and Process Engineering
Funding Number(s)
CONTRACT_GRANT: NNA15BB15C
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
3D weaving
thermal protection system
ablative
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