Rocket engine member and a method for manufacturing a rocket...

Power plants – Reaction motor – Including heat exchange means

Reexamination Certificate

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Details

C239S127100, C029S890010, C029S890140

Reexamination Certificate

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06920750

ABSTRACT:
Method and arrangement for providing liquid fuel rocket engine member (10). The member forms a body of revolution having an axis of revolution and a cross section that varies in diameter along said axis. The wall structure includes a plurality of cooling channels (11). The outside of the wall structure includes a continuous sheet metal wall (14). The cooling channels (11) are longitudinally attached to the inside of the sheet metal wall. The method for manufacturing the rocket engine member (10) includes the steps of forming a sheet metal wall (14) having a wall section corresponding to the desired nozzle section, providing a plurality of channel members (15), and attaching the channel members (15) to the inside of the sheet metal wall (14).

REFERENCES:
patent: 2968918 (1961-01-01), Denison
patent: 3690103 (1972-09-01), Dederra et al.
patent: 4584171 (1986-04-01), Niino et al.
patent: 4924653 (1990-05-01), Oly
patent: 5546656 (1996-08-01), Hartman et al.
patent: 6467253 (2002-10-01), Haggander
patent: 904887 (1962-09-01), None
patent: WO 9529785 (1995-11-01), None

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