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SRB thermal curtain design supportImprovements in SRB Thermal Curtain were identified by thermal design featuring: selection of materials capable of thermal protection and service temperatures by tri-layering quartz, S2 glass, and Kevlar in thinner cross section; weaving in single piece (instead of 24 sections) to achieve improved strength; and weaving to reduce manufacturing cost with angle interlock construction.
Document ID
19940012651
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Dixon, Carl A. (Southern Research Inst. Birmingham, AL, United States)
Lundblad, Wayne E. (Southern Research Inst. Birmingham, AL, United States)
Koenig, John R. (Southern Research Inst. Birmingham, AL, United States)
Date Acquired
September 6, 2013
Publication Date
November 1, 1992
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
SRI-MME-92-564-7079
NAS 1.26:193858
NASA-CR-193858
Accession Number
94N17124
Funding Number(s)
CONTRACT_GRANT: NAS8-38261
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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