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Stress corrosionThis article recounts briefly some of the more critical stress-corrosion failures that have been experienced at Marshall Space Flight Center and the corrective action taken. Some of the recent stress corrosion studies are described and preliminary results tabulated. Specific problems described are the H-1 Engine LOX dome, the pneumatic line fitting sleeve problems and the more recent problem with wave springs used on MF-flared tube fittings. The use of nitric oxide in preventing stress-corrosion failures in titanium tanks is also discussed.
Document ID
19670020054
Acquisition Source
Marshall Space Flight Center
Document Type
Contribution to a larger work
Authors
Charles E. Cataldo
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Date Acquired
August 3, 2013
Publication Date
January 1, 1966
Publication Information
Publication: Research Achievements Review
Publisher: Marshall Space Flight Center
Volume: 2
Issue: 4
Subject Category
Materials, Metallic
Report/Patent Number
N67-29383
Accession Number
67N29383
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
HIGH STRENGTH ALLOY
STRESS CORROSION
FAILURE
CORROSION PREVENTION
SATURN I /SA-1/ LAUNCH VEHICLE
SPACECRAFT COMPONENT
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