NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Brazed Borsic/aluminum structural panelsA fluxless brazing process has been developed that minimizes degradation of the mechanical properties of Borsic/aluminum composites. The process, which employs 718 aluminum alloy braze, is being used to fabricate full scale Borsic/aluminum-titanium honeycomb-core panels for Mach 3 flight testing on the YF-12 aircraft and ground testing in support of the Supersonic Cruise Aircraft Research (SCAR) Program. The manufacturing development and results of shear tests on full scale panels are presented.
Document ID
19770011276
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Bales, T. T. (NASA Langley Research Center Hampton, VA, United States)
Wiant, H. R. (Vought Corp. Hampton, Va., United States)
Royster, D. M. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
March 1, 1977
Subject Category
Composite Materials
Report/Patent Number
L-11075
NASA-TM-X-3432
Report Number: L-11075
Report Number: NASA-TM-X-3432
Accession Number
77N18220
Funding Number(s)
PROJECT: RTOP 743-01-22-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available