An energy attenuating apparatus for use with a seat includes an elongated attenuator having a resistance to bending which varies along its length. A bending mechanism defining a nonlinear path receives the attenuator. Translation of the bending mechanism relative to the attenuator in a lengthwise direction of the attenuator produces bending of the attenuator to absorb energy applied to the energy attenuating apparatus.

 
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> Apparatus with helical tension cables for ejecting a spin-stabilized body from a spacecraft

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