Solar reflector systems and methods

Aeronautics and astronautics – Spacecraft – With payload accommodation

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136245, B64G 144

Patent

active

060505265

ABSTRACT:
A reflector system for a solar wing is provided in which adjacent reflector panels are inhibited from relative movement by coupling tethers. Each reflector panel rotates to be in a stored position adjacent a backface of a respective solar panel. From this stored position, each reflector panel then rotates to be in a deployed position in which it forms a reflection angle with a solar cell face of the respective solar panel. Because of the inhibition of the tethers, the reflector panels deploy together so that one of them does not move past another of them and damage its reflection surface. Upon deployment of a solar wing, a set of spring-biased reflector sheets are automatically urged to cover respective apertures which facilitate installation of restraint structures that maintain the solar wing in its stored configuration.

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