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Nondestructive Evaluation Methods for the Ares I Common BulkheadA large scale bonding demonstration test article was fabricated to prove out manufacturing techniques for the current design of the NASA Ares I Upper Stage common bulkhead. The common bulkhead serves as the single interface between the liquid hydrogen and liquid oxygen portions of the Upper Stage propellant tank. The bulkhead consists of spin-formed aluminum domes friction stir welded to Y-rings and bonded to a perforated phenolic honeycomb core. Nondestructive evaluation methods are being developed for assessing core integrity and the core-to-dome bond line of the common bulkhead. Detection of manufacturing defects such as delaminations between the core and face sheets as well as service life defects such as crushed or sheared core resulting from impact loading are all of interest. The focus of this work will be on the application of thermographic, shearographic, and phased array ultrasonic methods to the bonding demonstration article as well as various smaller test panels featuring design specific defect types and geometric features.
Document ID
20100017376
Acquisition Source
Marshall Space Flight Center
Document Type
Presentation
Authors
Walker, James
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 24, 2013
Publication Date
March 24, 2010
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
M10-0094
M10-0398
Report Number: M10-0094
Report Number: M10-0398
Meeting Information
Meeting: American Society for Nondestructive Testing Spring Research Symposium and Conference
Location: Williamsburg, VA
Country: United States
Start Date: March 22, 2010
End Date: March 26, 2010
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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