Thin-film solar reflectors deployable from an edge-stowed config

Aeronautics and astronautics – Spacecraft – With payload accommodation

Patent

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Details

136245, 136292, B64G 144

Patent

active

060170026

ABSTRACT:
Flexible, lightweight reflective sheets are positioned to concentrate solar radiation upon spacecraft solar panels. The sheets are held with inner and outer spring members which urge each sheet from a gathered edge-stowed configuration towards a deployed, planar configuration. The outer spring members further urge each fully extended sheet to rotate about an axis along the panel's edge in a direction away from the solar panel's face. Restraint members in the form of tethers limit this rotation to place the sheet in a stable deployed position and orientation chosen by design to reflect solar radiation onto the panel face. The increased incident radiation permits a reduction of the number of solar cells needed to satisfy a power requirement, and allows consequent savings in spacecraft cost and weight. The outer spring members are resilient, elongate members which flex to a stowed position behind a respective panel or inerleavably gather with the flexible sheet into a compact stowed configuration adjacent a panel edge.

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Sokolsky, Ilene, et al., "Thin Film Solar Concentrator", Naval Research Laboratory, thin flim pp. 1-8.

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