NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Thermographic Inspection of Metallic Honeycomb Sandwich StructuresThe X-33/VentureStar has a Thermal Protection System (TPS) consisting mainly of brazed metallic honeycomb sandwich structures. Inspection of these structures is changing as a result of the extremely thin (less than 200 microns) skins, the small critical defect size (less than 2 mm long by 100 microns wide) and the large number (more than 1000) of parts to be inspected. Pulsed Infrared Thermography has been determined to be the most appropriate inspection method for manufacturing inspection based on performance comparison with other methods, cost, schedule and other factors. The results of the assessment of the different methods will be summarized and data on the performance of the final production inspection system will be given. Finite difference thermal methods have been used to model the whole inspection process. Details of correlation between the models and experimental data will be given and data on the use of pulsed infrared thermography on other metallic honeycomb sandwich structures will be given.
Document ID
19980236443
Acquisition Source
Marshall Space Flight Center
Document Type
Reprint (Version printed in journal)
Authors
Taylor, John O.
(Goodrich (B. F.) Aerospace Chula Vista, CA United States)
Dupont, H. M.
(Goodrich (B. F.) Aerospace Chula Vista, CA United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1998
Subject Category
Quality Assurance And Reliability
Meeting Information
Meeting: Annual Review of Progress in Quantitative Nondestructive Evaluation
Location: Snowbird, UT
Country: United States
Start Date: July 19, 1998
End Date: July 24, 1998
Funding Number(s)
CONTRACT_GRANT: NCC8-115
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available