Research, Design, Manufacture Cooling System for Test Chamber

The current equipment and materials used in UAV manufacturing have only been tested under normal conditions while UAVs operate in a wide range of environment conditions. Many UAVs fly at high altitude where the temperature drops significantly. Low ambient temperature will affect the operation of electronic components and structure of the UAVs. Therefore, it is very important to study the simulated low temperature environment equivalent to the operating condition of the UAV to check the operability, structural strength, and minimize the risk of damage and destruction of the UAV. This paper focuses on research, analysis, building principles, deployment of design diagrams, test chamber simulation and fabrication that have relatively controlled cooling rates based on the spread of cooling liquids.