Aerospace and Propulsion
Environmental chambers and anechoic chambers, as follows:
| Reference | Parameter | Threshold |
|---|---|---|
| 9B106.a | of the following flight conditions: a. Altitude equal to or | > 15 km |
| 9B106.a | est equipment to produce vibration environments equal to or | > 10 g rms |
| 9B106.a | between 20 Hz and 2 kHz while imparting forces equal to or | > 5 kN |
| 9B106.a | ulating any of the following flight conditions: a. Altitude | >= 15 km |
| 9B106.a | vibration test equipment to produce vibration environments | >= 10 g |
| 9B106.a | between 20 Hz and 2 kHz while imparting forces | >= 5 kN |
| 9B106.b | and 2. Altitude equal to or | > 15 km |
| 9B106.b | and 2. Altitude | >= 15 km |
9B106.aEnvironmental chambers having all of the following: 1. Capable of simulating any of the following flight conditions: a. Altitude equal to or greater than 15 km; or b. Temperature range from below 223 K (– 50 °C) to above 398 K (125 °C); and 2. Incorporating, or ‘designed or modified’ to incorporate, a shaker unit or other vibration test equipment to produce vibration environments equal to or greater than 10 g rms, measured ‘bare table’, between 20 Hz and 2 kHz while imparting forces equal to or greater than 5 kN;
9B106.bEnvironmental chambers capable of simulating the following flight conditions: 1. Acoustic environments at an overall sound pressure level of 140 dB or greater (referenced to 20 μPa) or with a total rated acoustic power output of 4 kW or greater; and 2. Altitude equal to or greater than 15 km; or 3. Temperature range from below 223 K (– 50 °C) to above 398 K (125 °C).
Decontrol note
Ne s’applique pas aux chambres environnementales destinées exclusivement à des applications civiles, telles que l’automobile ou l’électronique grand public.
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