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BSM Delta Qualification 2, volume 3, book 2This report, presented in three volumes, provides the results of a two-motor Delta Qualification 2 program conducted in 1993 to certify the following enhancements for incorporation into booster separation motor (BSM0 flight hardware: vulcanized-in-place nozzle aft closure insulation; new iso-static ATJ bulk graphite throat insert material, adhesive EA9394 for bonding the nozzle throat, igniter grain rod/centering insert/igniter case; deletion of the igniter adapter insulator ring; deletion of the igniter adapter/igniter case interface RTV; and deletion of loctite from igniter retainer plate threads. The enhancements above directly resulted from (1) the BSM total quality management (TQM) team initiatives to enhance the BSM producibility, and (2) the necessity to qualify new throat insert and adhesive systems to replace existing materials that will not be available. Testing was completed at both the component and motor levels. Component testing was accomplished to screen candidate materials (e.g., throat materials, adhesive systems) and to optimize processes (e.g., aft closure insulator vulcanization approach) prior to their incorporation into the test motors. Motor testing--consisting of two motors, randomly selected by USBI's on-site quality personnel from production lot AAY, which were modified to accept the enhancements -- was completed to provide the final qualification of the enhancements for incorporation into flight hardware. Volume 3, Book 2 provides various supporting documentation to the previous volumes with regards to the testing of the two Delta qualification units: data acceptance records, thermal conditioning analysis, igniter adapter thermal flake analysis, laboratory adhesive (EA-9394) qualification report, throat insert thermal/structural analysis, Delta Qualification Nonconformance Reports (NCR's), O-ring seating tests, and interim test report for vulcanization process qualification.
Document ID
19950018434
Acquisition Source
Legacy CDMS
Document Type
Book
Date Acquired
September 6, 2013
Publication Date
November 11, 1994
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
CSD-5597-93-2
NAS 1.26:196568
NASA-CR-196568
Report Number: CSD-5597-93-2
Report Number: NAS 1.26:196568
Report Number: NASA-CR-196568
Accession Number
95N24854
Funding Number(s)
CONTRACT_GRANT: NAS8-36300
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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