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Braze alloy process and strength characterization studies for 18 nickel grade 200 maraging steel with application to wind tunnel modelsA comprehensive study of braze alloy selection process and strength characterization with application to wind tunnel models is presented. The applications for this study include the installation of stainless steel pressure tubing in model airfoil sections make of 18 Ni 200 grade maraging steel and the joining of wing structural components by brazing. Acceptable braze alloys for these applications are identified along with process, thermal braze cycle data, and thermal management procedures. Shear specimens are used to evaluate comparative shear strength properties for the various alloys at both room and cryogenic (-300 F) temperatures and include the effects of electroless nickel plating. Nickel plating was found to significantly enhance both the wetability and strength properties for the various braze alloys studied. The data are provided for use in selecting braze alloys for use with 18 Ni grade 200 steel in the design of wind tunnel models to be tested in an ambient or cryogenic environment.
Document ID
19910015969
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Bradshaw, James F.
(NASA Langley Research Center Hampton, VA., United States)
Sandefur, Paul G., Jr.
(Lockheed Engineering and Sciences Co. Hampton, VA., United States)
Young, Clarence P., Jr.
(North Carolina State Univ. Raleigh., United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1991
Subject Category
Metallic Materials
Report/Patent Number
NAS 1.15:104075
NASA-TM-104075
Report Number: NAS 1.15:104075
Report Number: NASA-TM-104075
Accession Number
91N25283
Funding Number(s)
PROJECT: RTOP 505-59-85-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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