The Partial Pressure of Oxygen also defined as pressure exerted by oxygen component of air decreases in direct proportion to air pressure, while the altitude increases it become more difficult for humans to inhale oxygen which unfortunately if prolonged cause hypoxia and eventually death. To avoid hypoxia oxygen monitoring & controlling system in military aircraft maintains minimum Partial Pressure of Oxygen equivalent of sea level. Hence it is very important that reliability of such lifesaving system is uncompromised but how? Well, it’s CME! Time and again our state of art Altitude Chambers have stood on its reputation of the most preferred in defence industry for such sophisticate reliability testing.

Aircraft and its components are subject to extreme pressure and climatic conditions during flights. These parameters have a significant influence on the functioning of individual components, and they must be monitored and measured for safety reasons. CME Altitude chamber allow for the testing of aerospace components in an environment with controlled pressure, temperature and humidity parameters. An altitude of 100,000 feet [10 mbar] can be simulated in the test space.

BOD Incubators are designed to provide precise temperature control for applications such as microbial culture, BOD testing, or other research purposes, meeting stringent industry standards.

CATH chamber can simulate pressure, temperature and humidity in its test space. It is also known as combined altitude, temperature and humidity chamber which is primarily used in R&D and testing of aerospace components. The chamber meets many international standards including MIL and RTCA. The standard range of the CATH chamber includes 540 L , 1000 L and 1500 L while we also offer custom sizes as per customer requirement.