This invention relates to the field of material performance testing technology and discloses a
radar temperature
shock testing device, including a temperature
shock testing chamber and a testing cavity formed on the side of the chamber. The chamber is used for testing the physical and electrical properties of
radar materials and components under temperature shock. An air outlet is provided on the inner side of the testing cavity, and an air guide
assembly is provided on the inner wall to prevent high and low temperature airflows from directly blowing onto the
radar under test. In this invention, a portion of the
airflow enters the exhaust hood through the connecting shell, driving the fan blades to rotate and then being evenly discharged from three exhaust hoods in multiple directions. Another portion of the
airflow causes the air guide cloths of different lengths to oscillate irregularly, further dispersing the
airflow. This dual airflow guidance avoids the direct and forceful blowing of high and low temperature airflows onto the radar components, eliminating the influence of airflow interference on material performance testing, ensuring the authenticity and
repeatability of sample
test data under temperature shock, and is suitable for the testing and analysis of the
thermal stability, fatigue characteristics, and electrical properties of radar materials.