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Reuseable lightweight modular multi-layer insulation for space shuttleThe adaptation of the Self Evacuating Multilayer Insulation System to the space shuttle orbiter liquid hydrogen tanks was investigated. Small scale material screening tests and subscale panel tests demonstrated the potential of the insulation to withstand the anticipated 100 flight cycles. The composition of the material and the process for producing the finished insulation are described. Results of the various tests to determine the durability of the material are presented.
Document ID
19730022151
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Burr, K. F.
(Union Carbide Corp. Tonawanda, NY, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1973
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-CR-121166
Report Number: NASA-CR-121166
Accession Number
73N30883
Funding Number(s)
CONTRACT_GRANT: NAS3-14366
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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