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A space-based solar operated power module is configured for storage aboard a shuttle and then automatic deployment in the assigned orbit. It includes an articulated base support which is coupled to the ship\s frame during deployment, and a chassis module, which also serves as a housing for electrica

A space-based solar operated power module is configured for storage aboard a shuttle and then automatic deployment in the assigned orbit. It includes an articulated base support which is coupled to the ship\s frame during deployment, and a chassis module, which also serves as a housing for electrical components of the power supply, and which is connected to the base support. A pair of oppositely extended foldable arms are movably mounted on the chassis sides and each carries an assembly of collapsible solar panels for converting incident radiant energy to electrical energy. The chassis also supports radiator panels which extend from the top of the chassis in the craft\s vertical plane. At the start of deployment the shuttle\s remote controlled cargo arm is used for lifting the chassis and its appendages from the hold of the ship. A trapeze and ring assembly along with a berthing adapter, forming a part of the base support, are then used for engaging the chassis to the shuttle\s frame and moving the chassis to an overhead position. The solar panel assemblies, still folded, are then rotated outboard 90 degrees. The foldable arms, configured as linkages, thereafter expand outwardly from the side of the chassis for deployment of the solar panel assemblies. The entire station is then moved to a forward position after which the panel assemblies are unfurled.

대표청구항 ▼

A solar operated power station for space operation transportable in a spacecraft having a hold with a deck, said power station comprising: a chassis module containing electrical components and circuits of said station and drive system; articulated base support means movably interconnecting said chas

A solar operated power station for space operation transportable in a spacecraft having a hold with a deck, said power station comprising: a chassis module containing electrical components and circuits of said station and drive system; articulated base support means movably interconnecting said chassis and said spacecraft to guide the displacement of said chassis from said craft; a pair of opposing extensible arms each movably connected at its inboard end to a corresponding side of said chassis for operation by said drive system and extensible outwardly from said chassis side when driven by said drive system, each of said arms having two members and each of said members having two links pivotally interconnected to each other to form a scissor linkage; panel support tubes rotatably mounted transversely of each arm at an outboard end thereof, said panel support tubes being configured to be driven by said drive system when said arms are folded against the chassis sides; and an assembly of solar panels supported by each of said panel support tubes, each of said solar panel assemblies being configured for packing in a stowed position and including extender means for depolying solar cells of said panel assembly from a retracted position adjacent said chassis to a fully extended position for intercepting rays of sunlight, said tubes being secured to said arms for rotation of said solar panel assemblies from a position pointing toward the deck of the hold during stowage to an outwardly extending position after said chassis has been positioned.