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. • The low-pressure test chamber is also designed to meet many stringent MIL STD and RTCA test requirements. Sonacme Technology provides high and low temperature and low air pressure test chambers for simultaneous temperature/altitude testing from on-site altitude to 65,000 feet. • DEF STAN 0035 3-11 (High temperature, low pressure) • DEF STAN 0035 3-12 (High temperature, low pressure) • DEF STAN 0035 3-13 (low temperature and pressure) • MIL-STD-810G METHOD 500.5 Procedure I • MIL-STD-810G METHOD 500.5 Procedure II • MIL-STD-810G METHOD 500.5 Procedure III • RTCA/DO-160C 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.