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Vacuum / Pressure Test

Negative pressure or positive pressure tests are performed to simulate high altitudes or immersion in water with immersion simulations. They are preferably used for aerospace parts (altitude test).

Climbing and descending flights with constant pressure are used to test the transport of air cargo. Devices that are subjected to pressure fluctuations are tested by a rapid pressure difference (Rapid Decompression), while some devices have to prove their suitability by flying out of flaps in milliseconds (Explosive Decompression). Airborne altitudes of up to 30km above sea level can be simulated. The additional influence of cold air down to -55°C can thus result in a true-to-life simulation at high altitude.

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Vacuum/Pressure Test  Standards

  • JESD22-A102-C
  • MIL-STD-810
  • RTCA DO160 Sec. 4
  • RTCA DO160 Sec. 24
  • AECTP 300 Method 312
  • EN 60068-2-13
  • EN 60068-2-39
  • EN 60068-2-40
We also offer the following tests, among others:
engine
according to the following standards, among others:

  • DIN EN 2591-403
  • DIN EN 60068-2-6
  • 61373
  • DIN SPEC 79009
  • MIL-STD-810H
  • RTCA DO-160

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Vibration Tests
pressure chamber, vacuum chamber
according to the following standards, among others:

  • JESD22-A102-C
  • MIL-STD-810
  • DIN EN 62133-2 (VDE 0510-82)
  • RTCA DO160
  • AECTP 300
  • EN 60068-2-40

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Vacuum Tests
icing
according to the following standards, among others:

  • MIL-STD 810H
  • NEMA 250
  • RTCA DO-160G

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Icing Tests