Rocket engine combustion chamber

Details Rocket engine combustion chamber Rocket engine combustion chamber

1990-10-24

1992-04-14

Bertsch, Richard A.

Power plants

Reaction motor

Solid propellant

428610, F02K 900

Patent

active

051036371

ABSTRACT:
A rocket engine combustion chamber is defined by a generally cylindrical member comprising a metal matrix and heat insulating particles wherein the particles are distributed in the matrix such that the amount of particles gradually decreases in a radial direction from the inner surface to the outer surface of the member. Such a member is manufactured by controlled composite electroplating.

REFERENCES:
patent: 5038561 (1991-08-01), Chase

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