MIL MIL-STD-202/212 – Method 212, Acceleration
This test is performed for the purpose of determining the effects of acceleration stress on component parts, and to verify the ability of the component parts to operate properly during exposure to acceleration stress such as would be experienced in aircraft, missiles, etc.
Product Details
- Published:
- 04/18/2015
- Number of Pages:
- 5
- File Size:
- 1 file , 86 KB
- Note:
- This product is unavailable in Ukraine, Russia, Belarus
