Impact damage is of critical concern in structures using laminated fibre re
inforced composites. Thermoplastic polycarbonate (PC) offers high impact re
sistance and is often used in a variety of applications, including the wind
shield and canopy of aircraft, pressure windows and automotive parts among
others. Impact damage to structures utilizing composites has been an area o
f constant concern. In the current study, S2-glass/epoxy composite laminate
s bonded to PC (referred to as 'S2-glass/epoxy-PC' or 'Laminate-PC') have b
een investigated for their high strain rate (HSR) impact response. A compre
ssion Split Hopkinson Pressure Bar (SHPB) with 19.05 mm (0.75") incident an
d transmission bars with dynamic recovery technique was used to test four,
six and eight layers S2-glass/epoxy-PC samples. Using dynamic recovery tech
nique on the SHPB, the sample was subjected to a controlled single compress
ive pulse, providing information on damage evolution. The samples were test
ed under HSR impact in three directions (with respect to the side facing th
e incident bar of the SHPB). In the first, the PC faced the incident bar, i
n the second, the S2-glass/epoxy laminate faced the same, whereas in the th
ird, the loading was in the in-plane direction of the laminate. The HSR imp
act tests were performed by considering three strain rates - 109, 327 and 5
44/s - for all the experiments. The results of the investigation showed tha
t providing a PC facing to S2-glass/epoxy laminate is an effective way of o
btaining deformation in the PC facing which absorbs a large portion of the
incident energy, thereby minimizing any delamination threat to the composit
e backing. PC acts as a sacrificial layer that can be readily replaced in t
he application.