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Phased Array Ultrasonic Evaluation of Space Shuttle Main Engine (SSME) Nozzle WeldThis viewgraph presentation gives an overview of the phased array ultrasonic evaluation of the Space Shuttle Main Engine (SSME) nozzle weld. Details are given on the nondestructive testing evaluation approach, conventional shear wave and phased array techniques, and an x-ray versus phased array risk analysis. The field set-up was duplicated to the greatest extent possible in the laboratory and the phased array ultrasonic technique was developed and validated prior to weld evaluation. Results are shown for the phased array ultrasonic evaluation and conventional ultrasonic evaluation results.
Document ID
20020022677
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
James, Steve
(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)
Hopson, George
Date Acquired
September 7, 2013
Publication Date
January 1, 2001
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: 28th Review of Progress in Quantitative NDE Ultrasonic Transducer Arrays
Location: Brunswick, ME
Country: United States
Start Date: July 29, 2001
Funding Number(s)
CONTRACT_GRANT: NAS8-45000
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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