Design of an Auxiliary Equipment for Testability Test of Airborne Electronic Equipment

With the increasing thermal power consumption, heat flux per unit volume and surface area of airborne electronic equipment, testability test is faced with problem of ensuring different heat dissipation requirements of various airborne electronic equipment. Aiming at the heat dissipation requirements of different airborne electronic equipment, this paper designs an auxiliary equipment for testability test that integrates liquid cooling source and air-cooling source. The test auxiliary equipment provides a reference for the design of similar air-cooling source and liquid cooling source.