| 摘要 |
A method for deployment of a solar cell array, conduction of generated power from the array to the satellite, and utilization of the array and deployment means as an aid for the gravity-gradient stabilization of the satellite. The method envisions telescoping sections of a solar cell array being extended in orbit by an erectable mast and boom assembly. Power is carried from the array through electrically conductive booms and twin conducting masts, thereby eliminating the need for electrical wiring and associated wiring guides and connectors. The extended solar array also assists in stabilizing the satellite by providing necessary gravity-gradient restoring moments. Multiple function of equipment increases the wattage to weight ratio of the array.
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