NASA NTRS · 19720000592
Fabrication of cooled, graphite-lined structures
Abstract
Improved method of fabricating cooled graphite-lined thrust chamber has been developed. Layer of nickel is electrodeposited onto outer surface of machined and contoured graphite liner. Coolant passages are machined into nickel layer, filled with wax, outer shell electroformed over this, and wax removed. Tests in flox/methane rocket engine were completely successful.
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Duscha, R. A., Stubbs, V. R.. 1972-09-01. Fabrication of cooled, graphite-lined structures. https://ntrs.nasa.gov/citations/19720000592
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