Altitude Chamber
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.
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.
As rightly quoted “Good engineering is a perquisite for reliability”, a lot of detailing has gone in both the system designing and the component selection of the CME-AT series. These technologies require the utmost reliability of the components and systems on board, since human lives are often entrusted to them. Be it in refrigeration system comprising the semi hermetically sealed reciprocating compressor, high efficiency evaporator unit, in-built water-cooled condenser, on-Demand cooling, et all. are all carefully designed to offer the best reliability to the customer. The chamber can offer altitude ranges of up to 150,000 feet[1mbar] optionally as well. The Altitude chamber can also be customized as per the test requirements.
Model Selection table | |||||
CATH CHAMBER | |||||
Models | AT-225-B | AT-560-B | AT-1000-B | AT-1500-B | |
Test Space Dimension (WXDXH) |
mm | 500 x 400 x 600 | 780 x 800 x 940 | 1000 x 1000 x 1000 | 1000 x 1500 x 1000 |
inch | 20 X 16 X 24 | 31 x 31 x 37 | 39 x 39 x 39 | 39 x 59 x 39 | |
Test Space Volume | Ltr / Cuft | 225 / 8 | 560 / 20 | 1000 / 35.3 | 1500 / 53 |
Temperature Range* | (°C) (°F) |
– 60 to +120 -76 to +248 |
|||
Ramp rate** | (°C/min) | 1/2/3/5 | |||
Altitude range | mbar Ft |
Upto 10 [Default], 1 [Optional] Upto 100000 [Default], 150000 [Optional] | |||
* Optional Temperature Range also available | |||||
**Customized ramp rates are also available | |||||
CATH – Combined Altitude, Temperature and humidity chamber |