Altitude Control
Simulates low-pressure environments to mimic altitudes ranging from sea level to over 0.001 mbar. Essential for aerospace systems, avionics, and high-elevation applications.
A Combined Altitude, Temperature, and Humidity (CATH) test chamber is an advanced environmental simulation device used for rigorous testing of materials, components, and products under simultaneously controlled altitude, temperature, and humidity conditions. Widely used in aerospace, automotive, defence, and electronics industries to evaluate performance, durability, and reliability in extreme environments.
Advanced capabilities for replicating high-altitude, high-humidity and extreme thermal conditions in a single, repeatable cycle.
Simulates low-pressure environments to mimic altitudes ranging from sea level to over 0.001 mbar. Essential for aerospace systems, avionics, and high-elevation applications.
Recreates extreme heat and cold conditions across a wide thermal envelope — typically from −70 °C to +180 °C. Essential for thermal cycling and heat resistance testing.
Simulates relative humidity (RH) from 20 % to 98 %. Crucial for testing moisture-related performance issues such as corrosion, condensation, and material degradation.
Simultaneous control of all three parameters ensures accurate replication of real-world conditions — for example, high-altitude, high-humidity environments combined with extreme temperature variations.
Evaluating performance, durability and reliability under combined altitude, temperature and humidity stress.
Testing aircraft components, avionics, and materials for high-altitude and temperature extremes.
Evaluating the performance of devices like sensors and circuit boards in varying altitudes, temperatures, and humidity.
Testing vehicle components for operation at high elevations such as mountain driving conditions.
Ensuring military-grade equipment performs reliably under challenging environmental conditions.
Precision control across altitude, temperature and humidity — engineered for repeatable, standard-driven testing.
Sea level to over 0.001 mbar — simulating high-altitude and near-space low-pressure environments.
Typically from −70 °C to +180 °C for thermal cycling, heat resistance and cold-start evaluation.
Relative humidity from 20 % to 98 % — covering dry, humid, condensation and corrosion scenarios.
Simultaneous altitude, temperature and humidity control for realistic multi-parameter stress profiles.
Tell us your product, required test standard, chamber size, altitude range, temperature envelope and humidity requirements. Our team can help identify a suitable CATH testing configuration for your application.