Method of forming a rocket thrust chamber

Metal working – Method of mechanical manufacture – Rocket or jet device making

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Details

2989003, 295272, B23P 1500

Patent

active

061347825

ABSTRACT:
A method of making a rocket thrust chamber is described in which molten metal is sprayed onto the outer shell of a cooling tube bundle, and the ends of tubes are covered with predetermined thicknesses of the metal. Circumferentially extending manifold channels that intersect each of the tube ends are then machined into the predetermined thicknesses of metal, and mating assemblies are attached to enclose the manifold channels.

REFERENCES:
patent: 4584171 (1986-04-01), Niino et al.
patent: 5233755 (1993-08-01), Vandendriessche
patent: 5249357 (1993-10-01), Holmes et al.
patent: 5386628 (1995-02-01), Hartman et al.
patent: 5473817 (1995-12-01), Schnoor et al.
patent: 5477613 (1995-12-01), Bales et al.
patent: 5546656 (1996-08-01), Hartman et al.

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