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Qualification of the RSRM case membrane case-to-insulation bondline inspection using the Thiokol Corporation ultrasonic RSRM bondline inspection systemQualification testing of Combustion Engineering's AMDATA Intraspect/98 Data Acquisition and Imaging System that applies to the redesigned solid rocket motor (RSRM) case membrane case-to-insulation bondline inspection was performed. Testing was performed at M-67, the Thiokol Corp. RSRM Assembly Facility. The purpose of the inspection was to verify the integrity of the case membrane case-to-insulation bondline. The case membrane scanner was calibrated on the redesigned solid rocket motor case segment calibration standard, which had an intentional 1.0 by 1.0 in. case-to-insulation unbond. The case membrane scanner was then used to scan a 20 by 20 in. membrane area of the case segment. Calibration of the scanner was then rechecked on the calibration standard to ensure that the calibration settings did not change during the case membrane scan. This procedure was successfully performed five times to qualify the unbond detection capability of the case membrane scanner.
Document ID
19900013286
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Cook, M.
(Thiokol Corp. Brigham City, UT, United States)
Date Acquired
September 8, 2013
Publication Date
April 1, 1990
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NAS 1.26:183940
TWR-18898
NASA-CR-183940
Report Number: NAS 1.26:183940
Report Number: TWR-18898
Report Number: NASA-CR-183940
Accession Number
90N22602
Funding Number(s)
CONTRACT_GRANT: NAS8-30490
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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