specific power, excluding storage, of approximately 132 W/kg using 2.2 mil 13.5% silicon solar cells, a 2 mil cover glass and a 10% weight add-on for contingencies. The APSA wing is an ultra-lightweight flexible foldout blanket with a weight optimized deployment mechanism consisting of a fiberglass trilongeron lattice mast deployed from a cylindrical aluminum cannister and deployment actuator [29]. In the present case, specific powers were computed using the relation where ps is the array-specific power in W/kg, is the cell efficiency, I is AMO solar
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