The application provides a
spacecraft integrated active plate for non-uniform
heat flow devices and a manufacturing method thereof, comprising an active mounting plate, which comprises a thin-walled cavity, a mounting hole embedded part, a
heat pipe, a working medium filling hole and a space three-dimensional
crystal network sandwich structure; the mounting hole embedded part, the
heat pipe and the space three-dimensional
crystal network sandwich structure are arranged between the upper and lower walls of the thin-walled cavity; the mounting hole embedded part is used for mounting
electronic equipment; the array
cell of the space three-dimensional lattice network sandwich structure is in a Scherk's curved surface
cell configuration; the working medium filling hole is arranged on the side wall of the thin-walled cavity; and the thin-walled cavity, the mounting hole embedded part, the
heat pipe and the space three-dimensional
crystal network sandwich structure are integrally manufactured. The application solves the problems of large interface
thermal resistance, multi-point liquid leakage, poor
temperature control and uniform temperature effect in local
high heat flow area caused by the original SAR antenna active mounting plate gluing mode of more than 100 components, and meets the efficient
temperature control and uniform temperature demand of the SAR antenna intermittent working surface array uniform TR component.