A total of 27 Kevlar/epoxy truncated cones was manufactured and crushed und
er off-axis loads. Side loads were introduced by cutting the cones at angle
s relative to their central axes. The failure modes were observed, and the
specific sustained crushing stresses were determined and compared against g
raphite/epoxy cones of the same lay-up and similar geometry. The Kevlar/epo
xy cones exhibited significantly different failure modes than the graphite/
epoxy cones. Specifically, the cones did not experience brittle fracture, a
nd thus maintained structural integrity after crushing. The Kevlar/epoxy co
nes were less sensitive to the angle of the applied load than similar graph
ite/epoxy cones; however, the energy absorbed per unit mass is significantl
y lower. The role of specimen taper and load inclination is different than
that for graphite/epoxy cones. In particular, 10 degrees tapered cones over
all had the best performance even under uniaxial loading conditions.