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Phased Array Ultrasonic Examination of Space Shuttle Main Engine Nozzle WeldThis paper describes a Phased Array Ultrasonic Examination that was developed for the examination of a limited access circumferential Inconel 718 fusion weld of a Space Shuttle Main Engine Nozzle - Cone. The paper discusses the selection and formation criteria used for the phased array focal laws, the reference standard that simulated hardware conditions, the examination concept, and results. Several unique constraints present during this examination included limited probe movement to a single axis and one-sided access to the weld.
Document ID
20020048591
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
James, S.
(Boeing Co. Canoga Park, CA United States)
Engel, J.
(Boeing Co. Huntington Beach, CA United States)
Kimbrough, D.
(Boeing Co. Canoga Park, CA United States)
Suits, M.
(NASA Marshall Space Flight Center Huntsville, AL United States)
McCool, Alex
Date Acquired
September 7, 2013
Publication Date
January 1, 2001
Subject Category
Spacecraft Propulsion And Power
Funding Number(s)
CONTRACT_GRANT: NAS8-45000
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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