An energy storage includes a first container including an inner space, a plurality of pressure vessels for compressed air that are stacked in rows inside the inner space of the first container, a tank containing a heat transfer fluid arranged inside the inner space of the first container, a compressor adapted to compress air, and a plurality of pneumatic ducts for compressed air connected to the compressor. The plurality of pneumatic ducts includes a plurality of heat exchangers adapted to enable a heat exchange between compressed air contained in the plurality of pneumatic ducts and heat transfer fluid contained inside the tank. The plurality of pneumatic ducts is connected to the plurality of pressure vessels supplying pressure vessels with compressed air, an electric turbine connected by the plurality of pneumatic ducts with the plurality of pressure vessels supplying compressed air for rotating the electric turbine to generate electric current.

An energy storage includes a first container including an inner space, a plurality of pressure vessels for compressed air that are stacked in rows inside the inner space of the first container, a tank containing a heat transfer fluid arranged inside the inner space of the first container, a compressor adapted to compress air, and a plurality of pneumatic ducts for compressed air connected to the compressor. The plurality of pneumatic ducts includes a plurality of heat exchangers adapted to enable a heat exchange between compressed air contained in the plurality of pneumatic ducts and heat transfer fluid contained inside the tank. The plurality of pneumatic ducts is connected to the plurality of pressure vessels supplying pressure vessels with compressed air, an electric turbine connected by the plurality of pneumatic ducts with the plurality of pressure vessels supplying compressed air for rotating the electric turbine to generate electric current.

A system includes a plurality of storage brackets installed on a roof deck, each including a base plate, an arm and optionally a head and a receptacle. The arm is optionally rotatable. The receptacle of one of a first pair of storage brackets is configured to receive the head of another of the first pair of storage brackets. The receptacle of one of a second pair of storage brackets is configured to receive the head of another of the second pair of storage brackets. The first and second pairs of storage brackets are spaced apart from one another. The brackets are configured to receive at least one roofing material, which is positioned on the base plate of at least one of the first pair of brackets and at least one of the second pair of brackets.

A roll, comprising: a laminate, comprising: a plurality of solar cells, wherein the plurality of solar cells comprises: a first solar cell, a second solar cell, and a third solar cell, wherein the first solar cell and the second solar cell are separated in a first direction by a first distance, wherein the second solar cell and the third solar cell are separated in the first direction by the first distance, and wherein each of the first, second, and third solar cells comprises: a width in the first direction, and a length in a second direction, wherein the second direction is perpendicular to the first direction; a first encapsulant, wherein the first encapsulant encapsulates the plurality of solar cells, and wherein the first encapsulant includes a first surface and a second surface opposite the first surface; a frontsheet, wherein the frontsheet includes a first surface and a second surface opposite the first surface of the frontsheet, wherein the second surface of the frontsheet is adjacent the first surface of the first encapsulant; and a backsheet, wherein the backsheet includes a first surface and a second surface opposite the first surface of the backsheet, wherein the first surface of the backsheet is adjacent the second surface of the first encapsulant, and wherein the widths of the first, second, and third solar cells, and the first and second distances are sized to permit at least a portion of the first surface of the frontsheet to be juxtaposed circumferentially with at least a portion of the second surface of the backsheet.

A solar array assembly that includes a chassis, a top solar array assembly, a right side solar array assembly pivotable with respect to the chassis along a first horizontal axis, and a left side solar array assembly pivotable with respect to the chassis along a second horizontal axis. The right side solar array assembly includes a right central solar array assembly, a first right end solar array assembly pivotably connected to the right central solar array assembly about a first vertical axis, and a second right end solar array assembly pivotably connected to the right central solar array assembly about a second vertical axis. The left side solar array assembly includes a left central solar array assembly, a first left end solar array assembly pivotably connected to the right central solar array assembly about a third vertical axis, and a second left end solar array assembly pivotably connected to the right central solar array assembly about a fourth vertical axis.

A solar array assembly that includes a chassis, a top solar array assembly, a right side solar array assembly pivotable with respect to the chassis along a first horizontal axis, and a left side solar array assembly pivotable with respect to the chassis along a second horizontal axis. The right side solar array assembly includes a right central solar array assembly, a first right end solar array assembly pivotably connected to the right central solar array assembly about a first vertical axis, and a second right end solar array assembly pivotably connected to the right central solar array assembly about a second vertical axis. The left side solar array assembly includes a left central solar array assembly, a first left end solar array assembly pivotably connected to the right central solar array assembly about a third vertical axis, and a second left end solar array assembly pivotably connected to the right central solar array assembly about a fourth vertical axis.

The power generation module group 1 includes a sheet 10 and power generation panels 21 to 24. First lines L1 and L1′ are present between the panels 21 and 22 adjacent to each other in the lateral direction, the first lines crossing neither the panels 21 nor 22 and coming in contact with both the panels 21 and 22. The second line L2 is present on the bottom side of the panel 21 and on the bottom side of the panel 22, crosses neither the panels 21 nor 22 and is parallel in the lateral direction. An angle θ1 that is the largest angle on the panel 22 side of angles formed by the second line L2 and the first lines L1 and L1′ is an acute angle. The panels 23 and 24 are disposed in line symmetry with the panels 21 and 22, respectively, with respect to the lateral direction.

The power generation module group 1 includes a sheet 10 and power generation panels 21 to 24. First lines L1 and L1′ are present between the panels 21 and 22 adjacent to each other in the lateral direction, the first lines crossing neither the panels 21 nor 22 and coming in contact with both the panels 21 and 22. The second line L2 is present on the bottom side of the panel 21 and on the bottom side of the panel 22, crosses neither the panels 21 nor 22 and is parallel in the lateral direction. An angle θ1 that is the largest angle on the panel 22 side of angles formed by the second line L2 and the first lines L1 and L1′ is an acute angle. The panels 23 and 24 are disposed in line symmetry with the panels 21 and 22, respectively, with respect to the lateral direction.

Multi-functional coilable thin-walled structures that can be implemented within space-based satellite modules, and methods for their manufacture are provided. Multi-functional coilable thin-walled structures are comprised of at least one longeron that is capable of rolling and collapsing upon itself. In some embodiments, the coilable thin-walled longeron is a flange longeron. The flange longeron contains at least two major regions: a web and a plurality of flanges. The web region comprises portions of flanges that are bonded to one another. The plurality of flanges separate from one another on the same end of the web region. The plurality of flanges are similar in thickness and shape.

Provided is a method for relocating a solar power unit in response to a redeployment event. A first location of a deployed solar power unit may be determined. A processor may detect a redeployment event for the solar power unit at the first location. In response to the redeployment event, the processor may determine a new location for the solar power unit. The method may further comprise relocating the solar power unit to the new location.