Method of making rocket engine combustion chamber utilizing "sli

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

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Details

29428, B23P 1500

Patent

active

057016704

ABSTRACT:
A method of fabricating a rocket engine combustion chamber comprising assembling a liner having cooling channels, a plurality of throat support sections, and a structural jacket having inlet and outlet manifolds. Then heating the assembly in a pressurized furnace to bond the assembled parts to each other.

REFERENCES:
patent: 5226598 (1993-07-01), Woehrl
patent: 5386628 (1995-02-01), Hartman et al.
patent: 5501011 (1996-03-01), Pellet

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