Introduction:

The high-altitude environmental test chamber is an experimental device developed to meet the needs of aerospace and military equipment. It is used for ignition tests of satellite engines simulating high-altitude environments. During testing, the engine expels high-speed, high-temperature exhaust gas in pulses. The primary technical challenge in high-altitude simulation tests is to cool, extract, and discharge the high-temperature, high-speed exhaust gas into the atmosphere while maintaining a stable low-pressure environment inside the test chamber.

The high-altitude environmental test chamber can conduct plateau adaptability tests and plateau performance tests for electromechanical equipment. In medicine, it can be applied to high-altitude physiology, high-altitude sports training, and clinical disease treatment.

Technical Parameters:

The following specifications are for reference only and can be customized according to user requirements:

Simulated altitude: 100m to 30,000m

Temperature range: -60 to +85°C

Humidity range: 10% to 95% RH

Atmospheric pressure range: 1 kPa to 100 kPa

Oxygen supply range: Flow rate ≥ 350 L/min, Pressure: 0 to 0.6 MPa