| CPC F16B 33/004 (2013.01) [F16B 33/002 (2013.01); F16B 37/14 (2013.01); F16B 33/00 (2013.01)] | 20 Claims |

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1. A fastening system for aerospace vehicles comprising:
a dielectric nut retainer strip formed of dielectric material comprising at least one fastener thru hole and at least one cap receiver portion;
an anti-rotation nut retainer portion integrally formed in the dielectric nut retainer strip adjacent to the at least one fastener thru hole;
a cap configured to mate with the at least one cap receiver portion;
a fastener; and
an anti-rotation nut configured to fit in the anti-rotation nut retainer portion and couple with the fastener.
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