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NASA NTRS ยท 19950008386

Milestone 4: Thrust structure concepts and IHM screening Graphite Composite Primary Structure (GCPS)

Abstract

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.

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BibTeXRIS

Greenberg, H. S.. 1994-11-04. Milestone 4: Thrust structure concepts and IHM screening Graphite Composite Primary Structure (GCPS). https://ntrs.nasa.gov/citations/19950008386

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