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Milestone 4: Thrust structure concepts and IHM screening Graphite Composite Primary Structure (GCPS)The first part of the task was to select up to three promising thrust structure constructions and to select materials for screening tests. Part of the nondestructive evaluation and inspection (NDE/I) and integrated health management (IHM) task is to acquire and develop NDE/I sensor technologies and to integrate those sensors into the full scale test articles which will be produced under the TA2 program. Review of the anticipated fault modes and the available sensor technology data indicates that three sensor technologies should be assessed for the in-situ monitoring of the composite primary structure elements. These are: ultrasonics (dry contact), acoustic emissions, and fiber optics (embedded or attached). In fact, a combination of sensor technologies will be needed to detect and evaluate the fault modes; not only do sensor technology have specific capabilities and applicability, but the three Gr/Ep primary structures being demonstrated under the TA2 effort have differing requirements based on their respective failure modes and designs.
Document ID
19950008386
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Greenberg, H. S.
(Rockwell International Corp. Downey, CA, United States)
Date Acquired
September 6, 2013
Publication Date
November 4, 1994
Subject Category
Composite Materials
Report/Patent Number
NASA-CR-197053
SSD94D0328
NAS 1.26:197053
Report Number: NASA-CR-197053
Report Number: SSD94D0328
Report Number: NAS 1.26:197053
Accession Number
95N14800
Funding Number(s)
CONTRACT_GRANT: NCC1-193
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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