EVEREST – Altitude Test Chambers are specially designed for the testing of avionics aerospace and products which are exposed to high altitude conditions.
These simulators operate in a wide range of Temperature Altitude with user programmable rate of ascend and descend.
Optional models are available with humidity to perform the CATH Combined Altitude Temperature & Humidity cycle.
NAE, North American Envirosystems Altitude Test chambers are designed for simulating the actual conditions of high altitude to test various components, which may undergo low-pressure conditions especially in the avionics or aerospace industries.
Features:
- Temperature ranging from –70 deg C to 180 deg C with optional humidity.
- Altitude range up to 1 m bar.
- Digi-touch, touch screen controller with facilities of remote monitoring and operation, Internet Explorer based communication; Web enabled.
- Graphic Operator Interface, On-board communications and Built-in Ethernet.
- Square threaded durable locking arrangement for easy opening of door.
- Vacuum-sealed imported Teflon feed-through flanges will be provided for energizing the specimen during testing for variable power capacities.
- Vacuum sealed window with cyclic de-fog heaters.