Hybrid solar panel array

Aeronautics and astronautics – Spacecraft – With payload accommodation

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Details

74 8922, 16 82, 136292, 136265, B64G 144

Patent

active

057852804

ABSTRACT:
A hybrid solar panel array is mounted on a satellite sidewall for movement between a stowed position proximate the satellite sidewall and a deployed position extending away from the satellite sidewall. The array comprises a yoke pivotally mounted on the satellite sidewall and first and second rigid solar panels, the first panel being pivotally mounted to the yoke, the first and second panels being hinged together. In one embodiment, a plurality of semi-rigid solar panels are pivotally mounted to the first and second rigid solar panels. In another embodiment, a flexible solar panel is attached to the rigid solar panels. Drive mechanisms are operable for moving the array from a stowed position proximate a satellite sidewall to a deployed position extending away from the satellite sidewall. The rigid panels are so moved in a synchronous operation and the semi-rigid and flexible solar panels are so moved in a sequential operation.

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Proceedings of the First European Symposium on Photovoltaic Generators in Space, 11-13 Sep. 1978, Champion et al., "The ESA Lightweight Hybrid Solar Array", pp. 247-253.
Thirteenth IEEE Photovoltaic Specialists Conference, 5-8 Jun. 1978, Williams et al., "The ESA Lightweight Hybrid Solar Array" pp. 226-231.
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