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Improvement of Reusable Surface Insulation (RSI) materialsThe mullite fiber based hardened compacted fibers (HCF) type of reusable surface insulation was further developed for use in the Space Shuttle Program. Two hundred fifty formulations of fiber mixtures, fillers, binders, and organic processing aids were made using mullite fibers as the basic ingredient. Most of the work was accomplished on 15-lb/cu ft material. It was established that higher density materials are stronger with strength values as high as 250 lb/sq in. in tension. New measurement techniques and equipment were developed for accurate determination of strength and strain to failure. Room temperature to 2300 F stress-strain relationships were made. The room temperature tensile modulus of elasticity is 61,700 lb/sq in. and the strain at failure is 0.165 percent, typically, when measured longitudinally parallel to the long axes of the fibers. Thermal insulating effectiveness was increased 20 percent by reducing the diameter of some of the fibers in the material. Improvements were made in density uniformity and strength uniformity in a block of HCF by mixing improvements and by the use of organic additives. Specifications were established on the materials and processes used in making the insulation.
Document ID
19730008919
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Blome, J. C.
(McDonnell-Douglas Astronautics Co. Saint Louis, MO, United States)
Date Acquired
September 2, 2013
Publication Date
August 4, 1972
Subject Category
Materials, Nonmetallic
Report/Patent Number
MDC-E0647
NASA-CR-124053
Report Number: MDC-E0647
Report Number: NASA-CR-124053
Accession Number
73N17646
Funding Number(s)
CONTRACT_GRANT: NAS8-27688
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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