The invention relates to a high-performance
missile-borne
laser device. The high-performance
missile-borne
laser device comprises a shell, a containing cavity with an upper opening and a lower openingis formed in the shell, and an optical collimation lens, a
laser device collimation
assembly, a laser constant-power
driving circuit board, a first elastic pressing ring, a columnar battery and a second elastic pressing ring are sequentially arranged in the containing cavity from top to bottom. The bottom end of the shell is detachably provided with a bottom cover, and a screw hole aligned with the negative
electrode of the columnar battery is formed in the middle of the bottom cover. The containing cavity is filled with a filling and sealing material. The
missile-borne laser device is machined into an H shape through the shell, so that the
contact heat conduction area of the laser device and a
projectile body is greatly reduced, thermal
diffusion is reduced, and the laser device collimation
assembly is protected against
thermal shock of an external high-temperature environment. The optical collimation lens, the laser collimation
assembly, the laser constant-power
driving circuit board and the columnar battery are subjected to integrated
solid-state filling and sealing, the
crimp-type
electrode structure guarantees the overall firmness and reliability of the whole laser device, and the laser device is reasonable in structural design, stable in performance and resistant to vibration.