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Thermal blanket insulation for advanced space transportation systemsThe feasibility of weaving Nextel ceramic and Nicalon silicon carbide yarns into integrally woven, three dimensional fluted core fabrics was demonstrated. Parallel face fabrics joined with woven fabric ribs to form triangular cross section flutes between the faces were woven into three single and one double layer configuration. High warp yarn density in the double layer configuration caused considerable yarn breakage during weaving. The flutes of all four fabrics were filled with mandrels made from Q-Fiber Felt and FRCI-20-12 to form candidate insulation panels for advanced Space Transportation Systems. Procedures for preparing and inserting the mandrels were developed. Recommendations are made on investigating alternate methods for filling the flutes with insulation, and for improving the weaving of these types of fabrics.
Document ID
19870008472
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Pusch, Richard H.
(Woven Structures, Inc. Compton, CA, United States)
Date Acquired
September 5, 2013
Publication Date
February 1, 1985
Subject Category
Nonmetallic Materials
Report/Patent Number
NAS 1.26:177341
NASA-CR-177341
Report Number: NAS 1.26:177341
Report Number: NASA-CR-177341
Accession Number
87N17905
Funding Number(s)
PROJECT: RTOP 506-53-31
PROJECT: RTOP 506-63-39
CONTRACT_GRANT: NAS2-11718
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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