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Space Shuttle production verification motor 1 (PV-1) field joint protection system, volume 7The performance of the field joint protection system (FJPS) of the Space Shuttle Production Verification Motor 1 (PV-1), as evaluated by postfire hardware inspection. Compliance with the specifications is shown for the FJPS assembly and components. The simplified FJPS and field joint heaters performed nominally, maintaining all joint seal temperatures within the required range. One anomally was noted on the igniter-to-case joint heater during postfire inspection. The heater buckled off the surface in two areas, resulting in two hot spots on the heater and darkened heater insulation. The condition did not affect heater performance during ignition countdown and all igniter seals were maintained within required temperature limits.
Document ID
19910008895
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Wilkinson, J. P.
(Thiokol Corp. Brigham City, UT, United States)
Date Acquired
September 6, 2013
Publication Date
December 10, 1990
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NAS 1.26:184105
TWR-17592-VOL-7
NASA-CR-184105
Report Number: NAS 1.26:184105
Report Number: TWR-17592-VOL-7
Report Number: NASA-CR-184105
Accession Number
91N18208
Funding Number(s)
CONTRACT_GRANT: NAS8-30490
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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