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TP-H1148 knitline integrity evaluationThe main objective was to reevaluate the TP-H1148 propellant knitting capabilities due to minor changes in TP-H1148 raw materials and to test the effects of aging on the knitline and the bondline of the propellant to the liner (when epoxy primer was applied).
Document ID
19910008975
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Gill, M. (Thiokol Corp. Brigham City, UT, United States)
Date Acquired
September 6, 2013
Publication Date
November 1, 1990
Subject Category
Propellants And Fuels
Report/Patent Number
NASA-CR-184106
TWR-18755
NAS 1.26:184106
Accession Number
91N18288
Funding Number(s)
CONTRACT_GRANT: NAS8-30490
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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