Combustion chamber for rocket motor and its assembling method

Details Combustion chamber for rocket motor and its assembling method Combustion chamber for rocket motor and its assembling method

1987-01-21

1988-11-29

Casaregola, Louis J.

Power plants

Reaction motor

Solid propellant

60909, F02K 908

Patent

active

047872020

ABSTRACT:
Combustion chamber for rocket motor of the type comprising two domes, interconnected by a cylindrical shell, each of said domes and the intermediate shell being produced from a filamentary composite material, in which each dome comprises a slightly conical skirt of which the external face is joined over at least part of its length to the inner face of the shell, via a split cylindro-conical connection ring and at least opposite the conical skirt of the dome, one conical face having the same conicity as the conical skirt, the assembling of the three elements to be connected, i.e. dome, shell and ring, being achieved by adhesive bonding.

REFERENCES:
patent: 3173249 (1965-03-01), Wiggins
patent: 3243956 (1966-04-01), Hamm et al.
patent: 3296802 (1967-01-01), Williams
patent: 3812671 (1974-05-01), Burr et al.

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