CPC H01Q 15/02 (2013.01) [H01Q 3/14 (2013.01); H01Q 3/20 (2013.01); H01Q 1/288 (2013.01)] | 31 Claims |
1. A deployable electromagnetic radiation antenna system comprising:
one or more support structures;
an electromagnetic radiation directing lens adapted to pass a beam of electromagnetic radiation; and
a satellite body including at least one deployment mechanism, wherein the electromagnetic radiation directing lens is deployable in a first direction away from the satellite body, the electromagnetic radiation directing lens being coupled to the satellite body by the one or more support structures, wherein the at least one deployment mechanism deploys the one or more support structures by increasing the one or more support structures in length to extend between the electromagnetic radiation directing lens and the satellite body along the length, wherein increasing the one or more support structures in length causes concurrent expansion of the electromagnetic radiation directing lens from an undeployed state to a deployed state to at least form a substantially planar surface of the deployed electromagnetic radiation directing lens.
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