NASA NTRS · 19720007140
Advanced thrust chamber designs
Abstract
A regeneratively cooled thrust chamber has been designed and fabricated, consisting of an inner TD nickel liner which was spin formed, welded, and machined and an outer shell of electroformed nickel. Coolant channels were produced in the outer surface of the inner liner by the electric discharge machining process before electroforming the shell. Accessory manifolds and piping were attached by welding. Manufacturing processes employed are described.
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Dietrich, F. J., Leach, A. E.. 1971-07-01. Advanced thrust chamber designs. https://ntrs.nasa.gov/citations/19720007140
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