International Scholarly Research Notices / 2012 / Article / Fig 10

Research Article

The Self-Healing Capability of Carbon Fibre Composite Structures Subjected to Hypervelocity Impacts Simulating Orbital Space Debris

Figure 10

(a) Integration of 4–8 FBGs sensors embedded between 2nd and 3rd CFRP layer and concentrated inside a circle surface of 5 cm-diam. corresponding to the exposed area to debris during the hypervelocity impact experiment. (b) Final prototype of the sample.
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(a)
351205.fig.0010b
(b)
351205.fig.0010c
(c)