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Under controlled lab settings, two distinct laminates, one containing cenosphere and the other with neat resin, were evaluated for impact using a Fractovis impact machine, compression testing, and compression after impact tests (CAI) with a Tinus Olsen UTM. The GFRP laminates were made by hand lay-up method with 16 layers of glass fiber in 4.7±0.2 mm thickness and combined with epoxy resin reinforced Cenospheres at concentrations of 1, 3 and 5 wt. %, according to ASTM specifications. The dominant failure mode controlling the specimen's compression ultimate load resistance, and other failure modes of impacted specimens such like fiber pull-out and debonding, were found to be the effects of delamination using coupled acoustic emission (AE) monitoring and compression tests. On specimens with a 3 wt. % filler additive, there was a noticeable increase in strength. Both impacted and non-impacted samples exhibited significant compression ultimate load resistances, with the 3 wt. % filler impregnated specimen having the maximum.

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