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Development of sputtered techniques for thrust chambersThe 0.152 cm thick sputtered and copper deposits were electron beam welded to wrought copper. Tensile specimens were machined from the weld assemblies and tested at room temperature. Tensile strength approached the strength of wrought material. Elongations up to 25% were measured. Sputtered aluminum was used to fill 0.157 cm wide by 0.127 cm deep grooves in thrust chamber spool piece liners. The liners were closed out by sputtering copper from post and hollow cathodes.
Document ID
19790024155
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Mullaly, J. R.
(Pratt and Whitney Aircraft Group West Palm Beach, FL, United States)
Allard, P. A.
(Pratt and Whitney Aircraft Group West Palm Beach, FL, United States)
Date Acquired
August 9, 2013
Publication Date
March 1, 1979
Subject Category
Metallic Materials
Report/Patent Number
NASA-CR-159637
FR-11409
Report Number: NASA-CR-159637
Report Number: FR-11409
Accession Number
79N32326
Funding Number(s)
CONTRACT_GRANT: NAS3-20377
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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