An aluminum honeycomb was filled with a rigid foam to improve its mech
anical properties. This foam-filled honeycomb was used to construct sa
ndwich panels with graphite/epoxy composite face sheets. The mechanica
l properties of the foam-filled honeycomb were found to be superior to
the unfilled honeycomb. Low velocity impact test results indicated th
at the sandwich panel containing the new core had much improved impact
resistance and that the impact-inflicted core crushing was highly loc
alized.