This paper analyzes the heat dissipation path of the high power components in aerospace electronic equipment. High thermal conductivity graphite sheet, accurately control of heat conduction pad compression and increase of heat conduction path are used for component which heat dissipation through the top. Covering the vias with copper are used for component which heat dissipates through the bottom. Combined with thermal simulation and temperature cycle test, the heat dissipation problem of high power component is effectively solved.