초록 ▼

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

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.

대표청구항 ▼

A rocket engine combustion chamber having a generally cylindrical member having an outer surface and an inner surface defining the combustion chamber, said member comprising a metal matrix having heat insulating particles distributed therein uniformly in a direction generally parallel to the surface

A rocket engine combustion chamber having a generally cylindrical member having an outer surface and an inner surface defining the combustion chamber, said member comprising a metal matrix having heat insulating particles distributed therein uniformly in a direction generally parallel to the surfaces, but in a radial direction such that the amount of particles gradually decreases from the inner surface to the outer surface.