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Leach, A. E.

Publications and source records attributed to Leach, A. E..

Advanced thrust chamber designs

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.

Dietrich, F. J.

Fabrication methods for TD nickel.

Spin-forming, welding, machining, electric discharge machining, and electroforming operations in th e construction of a TD Nickel rocket thrust chamber are described. TD Nickel was one of the first commercially available dispersion hardened alloys. Dispersion hardened alloys are being given prominent consideration in the construction of the space shuttle; therefore, fabrication experience gained with the TD Nickel material is of current interest.

Leach, A. E.