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Development of sputtered techniques for thrust chambersTechniques and materials were developed and evaluated for the fabrication and coating of advanced, long life, regeneratively cooled thrust chambers. Materials were analyzed as fillers for sputter application of OFHC copper as a closeout layer to channeled inner structures; of the materials evaluated, aluminum was found to provide the highest bond strength and to be the most desirable for chamber fabrication. The structures and properties were investigated of thick sputtered OFHC copper, 0.15 Zr-Cu, Al2O3,-Cu, and SiC-Cu. Layered structures of OFHC copper and 0.15 Zr-Cu were investigated as means of improving chamber inner wall fatigue life. The evaluation of sputtered Ti-5Al-2.5Sn, NASA IIb-11, aluminum and Al2O3-Al alloys as high strength chamber outer jackets was performed. Techniques for refurbishing degraded thrust chambers with OFHC copper and coating thrust chambers with protective ZrO2 and graded ZrO2-copper thermal barrier coatings were developed.
Document ID
19750021175
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Mullaly, J. R.
(Pratt and Whitney Aircraft West Palm Beach, FL, United States)
Hecht, R. J.
(Pratt and Whitney Aircraft West Palm Beach, FL, United States)
Schmid, T. E.
(Pratt and Whitney Aircraft West Palm Beach, FL, United States)
Torrey, C. T.
(Pratt and Whitney Aircraft West Palm Beach, FL, United States)
Date Acquired
September 3, 2013
Publication Date
March 1, 1975
Subject Category
Metallic Materials
Report/Patent Number
NASA-CR-134824
FR-6924
Report Number: NASA-CR-134824
Report Number: FR-6924
Accession Number
75N29248
Funding Number(s)
CONTRACT_GRANT: NAS3-17792
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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