NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Guidelines for Mapping Reliably Detectable Dye Penetrant Crack Size at External Corners with Fillet RadiiThe technical memorandum addresses some concerns with dye penetrant crack sizes stated in Table 1 (and Table 2) of NASA-STD-5009B. Table 1 corner crack size of a = 0.100” and c = 0.150” is reasoned to be larger than it should be based on the original Standard dye penetrant qualification. In the original Standard dye penetrant qualification, surface crack size with depth a = 0.075” x length 2c = 0.150” was qualified with minimum 90% Probability of Detection (POD) with 95% confidence (conf.). No corner crack size was qualified by direct POD testing in original dye penetrant qualification. Standard dye penetrant detectable crack size for radiused corner is not addressed in NASA-STD-5009B.
Document ID
20230000318
Acquisition Source
Johnson Space Center
Document Type
Technical Memorandum (TM)
Authors
Ajay M. Koshti
(Johnson Space Center Houston, Texas, United States)
David M. Stanley
(Jacobs (United States) Dallas, Texas, United States)
Nathan Trepal
(Kennedy Space Center Merritt Island, Florida, United States)
James L. Walker
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Date Acquired
January 10, 2023
Publication Date
February 1, 2023
Subject Category
Quality Assurance and Reliability
Funding Number(s)
WBS: 484997.01.01.01.02.01
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Technical Management
Keywords
Dye Penetrant Testing
Nondestructive Testing
No Preview Available