Altitude test chamber SAT/xxx/70(H) series

climatictemperaturepressure

The high, low temperature and low pressure altitude test chamber (temperature/altitude) is designed to allow users to perform temperature and altitude condition tests in a combined test chamber, and create multiple conditions to meet multiple test requirements at the same time. For the test application of satellites, rockets, airplanes or helicopters: modern airplanes are subject to great pressure during use. We provide prefabricated and customized low-pressure test chambers for ultra-low cooling and extended temperature range to meet your exact test requirements. Structural Features • The inner chamber is fully welded from 2mm thick SUS304 stainless steel plate. The advantage of full welding is that it has good sealing and is not easy to crack. • The outer wall adopts 10mm thick HRS steel plate, and adopts a detachable plate structure in the appropriate position, which is convenient for future maintenance and repair of the insulation interlayer of the cabinet; the metal plate is cleaned and treated with corrosion-resistant and anti-rust paint. • The insulation material is made of polyurethane automatic mechanical foaming, and the thickness of the insulation layer is 150 mm. • The door is sealed with double-layer silicone sealing material, which has a good sealing effect. Electrical System • The overall layout of the circuit cabinet looks very neat and professional. Our circuits are arranged in accordance with UK standards and are equipped with complete circuit diagrams. Each line has a unique code which is clearly defined and easy to locate for troubleshooting.