Aeronautics

Altitude tests over the years have become increasingly more complex and integrated. The ability to control numerous parameters at the same time (such as altitude, temperature and relative humidity) are now characteristic of the standard altitude test chamber. Aviation technologies require the utmost of reliability since lives are entrusted. It is therefore necessary to conduct tests to simulate operating conditions in both ordinary procedure and the at the Quality Control and Production levels.

The standard chamber in question is able to comply not just with the most common international standards of the sector, but is also designed to meet the most selective demands in the market. The parameters of altitude, temperature and relative humidity are all incorporated within the same chamber making the simulation of extreme changes of conditions on the tested aircraft components possible.

We have designed and developed a complete series of standard chambers for vacuum tests up to 1 mbar (equivalent to 150,000 feet altitude). A special wall thermoregulation system (optional) guarantees the best functioning below 300 mbar, with the test environment thermoregulated by radiation. This range of altitude chambers is also available in both thermostatic (temperature and pressure control) and climatic (temperature, pressure, and humidity control) versions.