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Lightweight Thermal Protection System for Atmospheric EntryTUFROC (Toughened Uni-piece Fibrous Reinforced Oxidation-resistant Composite) has been developed as a new thermal protection system (TPS) material for wing leading edge and nose cap applications. The composite withstands temperatures up to 1,970 K, and consists of a toughened, high-temperature surface cap and a low-thermal-conductivity base, and is applicable to both sharp and blunt leading edge vehicles. This extends the possible application of fibrous insulation to the wing leading edge and/or nose cap on a hypersonic vehicle. The lightweight system comprises a treated carbonaceous cap composed of ROCCI (Refractory Oxidation-resistant Ceramic Carbon Insulation), which provides dimensional stability to the outer mold line, while the fibrous base material provides maximum thermal insulation for the vehicle structure.
Document ID
20100011117
Acquisition Source
Ames Research Center
Document Type
Other - NASA Tech Brief
Authors
Stewart, David
(NASA Ames Research Center Moffett Field, CA, United States)
Leiser, Daniel
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 24, 2013
Publication Date
October 1, 2007
Publication Information
Publication: NASA Tech Briefs, October 2007
Subject Category
Composite Materials
Report/Patent Number
ARC-15201-1
Distribution Limits
Public
Copyright
Public Use Permitted.
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