Non-standard Customization for Vacuum Environment Simulation Chamber--Lab Companion

Non-standard Customization for Vacuum Environment Simulation Chamber--Lab Companion

The various environmental and temperature factors at high altitude have a greater impact on the performance of raw materials, components and electromechanical products in physical, chemical, mechanical and electrical aspects of airplanes, airships and other vehicles at high altitude. In the process of vehicle research, the reliability test of high altitude climate environment must be carried out to ensure the safe and reliable operation of the equipment.

Functions and parameters

1) Temperature and humidity control: to meet the extreme temperature environment experienced by aviation vehicles operating in the inner atmosphere;

(2) Pressure control: the altitude changes experienced by the vehicle during flight;

(3) Solar radiation: the impact of solar radiation on materials and personnel experienced by the vehicle during flight;

1) Pressure range: atmospheric pressure ~ 1×10-9Pa;

2） Temperature range: -180℃～60℃;

3) Temperature accuracy: ±0.5℃;

4) Solar radiation: 1200W/m2;

5) Solar UV irradiance: 10-3W/cm2.

(All the above parameters can be customized according to the user's needs)