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Joining and fabrication of metal-matrix composite materialsManufacturing technology associated with developing fabrication processes to incorporate metal-matrix composites into flight hardware is studied. The joining of composite to itself and to titanium by innovative brazing, diffusion bonding, and adhesive bonding is examined. The effects of the fabrication processes on the material properties and their influence on the design of YF-12 wing panels are discussed.
Document ID
19750025110
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Royster, D. M. (NASA Langley Research Center Hampton, VA, United States)
Wiant, H. R. (LTV Aerospace Corp. Hampton, VA, United States)
Bales, T. T. (NASA Langley Research Center)
Date Acquired
September 3, 2013
Publication Date
October 1, 1975
Subject Category
Composite Materials
Report/Patent Number
NASA-TM-X-3282
L-10357
Report Number: NASA-TM-X-3282
Report Number: L-10357
Accession Number
75N33183
Funding Number(s)
PROJECT: RTOP 743-01-22-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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