Thermal Chamber

Our Space department’s Thermal Vacuum laboratory carries out research on aerospace-related thermal issues. The laboratory is equipped with various data acquisition /logging systems for different types of temperature and vacu-um/pressure sensors, and 50 Hz infrared camera.
Furthermore, single-phase and two-phase liquid/vapor heat transport systems can be developed and tested. To this end, a range of Coriolis mass flow meters, pumps, tubing and fittings are available. Fluid properties such as contact angle, surface tension and density can be measured with dedicated equipment.

Specimen length [mm]: 1200.0
Specimen width/dia [mm]: 1200.0
Specimen height/thk [mm]: 1200.0
Mass max. [kg]: 300.0
Higher temperature [K]: 573.0
Lower temperature [K]: 123.0
Temperature change rate [±K/min]: 40.0
Solar simulator intensity max. [W/m²]: 0
Feedthroughs: 2x generic holes of diameter 150 mm
Data acquisition: Fixed 6-channel Pt-100 data logging system, expandable with an independent data acquisition/logging system
Vacuum limit [hPa] [mbar]: Ambient
Cleanroom classes (ISO 14644-1):
ISO Class ≤5
ISO Class 6
ISO Class 7
ISO Class 8
ISO Class 9
Keywords: Cable harness TCT, aircraft components, NLR