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Experimental studies of confinement integrity of metal cask subjected to impulsive loads due to aircraft engine crash (Part.1)

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Academic year: 2020

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Figure

Figure 1. Considered Scenarios for Aircraft Engine Crash onto the Metal Cask without Impact Limiters
Figure 3. Relationship between Leak Rate and Siding Displacement of Scale Model
Figure 5. Overview of the Scale Model Cask
Figure 7 shows the measuring items. During the missile impact test, the acceleration and displacement of the lid and cask body, and the leak rate of the metal gasket were measured
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