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NASA NTRS · 19790024155

Development of sputtered techniques for thrust chambers

Abstract

The 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.

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BibTeXRIS

Mullaly, J. R., Allard, P. A.. 1979-03-01. Development of sputtered techniques for thrust chambers. https://ntrs.nasa.gov/citations/19790024155

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