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Fiber reinforced, shape memory, polymer matrix, composites have recently been demonstrated in a variety of applications. Once cured, these composites, based on thermoset shape memory resins, have the ability to be semi-permanently deformed from the cured shape at elevated temperatures and then subsequently returned to the original shape. However, the vast majority of the applications demonstrated have made use of very thin composite laminates. The current research considers composite sandwich panel structures formed from shape memory composite facesheets and a rigid foam core created from shape memory resin. The goal is to investigate the potential deformability in these much more rigid geometries to assess the potential for use in conformable, structural applications.

Predictive capabilities and understanding of how energy absorbing composite structures can be constructed, without additional size or weight, are necessary in order to ensure the deceleration of the driver is kept below human threshold levels. Often, the deceleration rate is modified by changes in the core or crushable material of the composite structure. In the current research, carbon fiber energy attenuators were designed, constructed, and tested to demonstrate the ability to tailor the energy absorbing profile through changes of the fiber orientation and ply stacking sequence. Reinforcing wraps of uni-directional carbon fiber were used to modify a baseline ply sequence and improved response was recorded in each case.