Large solar arrays with high natural frequencies

Aeronautics and astronautics – Spacecraft – With payload accommodation

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244158R, B64G 144

Patent

active

047875801

ABSTRACT:
A solar array structure for use with satellites requiring large areas of solar arrays. Each array is a single continuous structure having continuous longitudinal members which in a stowed condition enable the panel to be wrapped around the satellite within its launch vehicle. In a deployed configuration, the longitudinal members are reconfigured to provide substantially increased stiffness in the direction of winding.

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patent: 3606211 (1971-09-01), Roersch et al.
patent: 3863870 (1975-02-01), Andrews et al.
patent: 4133501 (1979-01-01), Pentlicki
patent: 4293731 (1981-10-01), Schweig et al.

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