SPACE-QUALIFIED SOLAR CELL ASSEMBLY COMPRISING SPACE-QUALIFIED SOLAR CELLS SHAPED AS A PORTION OF A CIRCLE
A space-qualified solar cell assembly comprising a plurality of space-qualified solar cells, each space-qualified solar cell of the plurality of space-qualified solar cells being shaped as a portion of a circle, the portion having at least one curved edge having a shape of the arc of the circumference of said circle and at least one straight edge, the portion having a surface area corresponding to not more than 50% of the surface area of the circle. This makes it possible to make efficient use of the material of the wafer from which the space-qualified solar cells are produced by reducing waste, while arrangement of the space-qualified solar cells into rectangular unit cells enables construction of substantially rectangular space-qualified solar cell arrays and assemblies that have their surface area covered substantially by space-qualified solar cells with little area unoccupied by space-qualified solar cells.
1 . A space-qualified solar cell assembly designed for operation at AM 0 and at a 1 MeV electron equivalent fluence of at least 5×10 14 e/cm 2 , the assembly comprising a III-V compound semiconductor multijunction solar cell including at least three subcells, including a ceria doped borosilicate glass supporting member that is 3 to 6 mils in thickness attached to each solar cell with a transparent adhesive, wherein a combination of compositions and band gaps of the subcells is designed to maximize efficiency of the solar cell at a predetermined end-of-life (EOL) time period, after initial deployment when the solar cell is deployed in space at AM 0 and at an operational temperature in the range of 40 to 70 degrees Centigrade, the predetermined EOL time period comprising at least five years, the space-qualified solar cell assembly comprising a plurality of space-qualified solar cells, each space-qualified solar cell of the plurality of space-qualified solar cells being shaped as a portion of a circle, the portion having at least one curved edge having a shape of an arc of a circumference of said circle and at least one straight edge, the portion having a surface area corresponding to not more than 50% of a surface area of said circle.
2 . The space-qualified solar cell assembly of claim 1 , wherein the curved edge of the plurality of space-qualified solar cells has a length corresponding to at least 45 degrees, preferably at least 60 degrees, more preferably at least 90 degrees, and up to 180 degrees of the circumference of the circle.
3 . The space-qualified solar cell assembly according to claim 1 , wherein the plurality of space-qualified solar cells are substantially shaped as sectors of circles.
4 . The space-qualified solar cell assembly of claim 3 , wherein the plurality of space-qualified solar cells comprises a plurality of space-qualified solar cells substantially shaped as quadrants of circles.
5 . The space-qualified solar cell assembly of claim 3 , wherein the plurality of space-qualified solar cells comprises a plurality of space-qualified solar cells shaped as semicircles.
6 . The space-qualified solar cell assembly of claim 3 , wherein the plurality of space-qualified solar cells comprises a plurality of space-qualified solar cells shaped as semicircles and quadrants of circles.
7 . The space-qualified solar cell assembly of claim 1 , wherein a plurality of the space-qualified solar cells are arranged so that a straight edge of one space-qualified solar cell is placed against the straight edge of another one of the space-qualified solar cells.
8 . The space-qualified solar cell assembly of claim 1 , wherein the space-qualified solar cells are arranged in a pattern formed by an array of rectangular unit cells, each unit cell encompassing a substantially identical arrangement of at least two space-qualified solar cells.
9 . The space-qualified solar cell assembly of claim 8 , wherein each unit cell encompasses at least two space-qualified solar cells arranged so that the curved edge of each one of said space-qualified solar cells is placed against the curved edge of another one of said space-qualified solar cells.
10 . The space-qualified solar cell assembly of claim 8 , wherein each unit cell encompasses at least two space-qualified solar cells arranged so that a flat portion at a curved edge of one space-qualified solar cell is placed against a flat portion at a curved edge of another one of said space-qualified solar cells.
11 . The space-qualified solar cell assembly of claim 1 , wherein the space-qualified solar cells have been obtained by dividing one or more substantially circular wafers into a plurality of substantially identical portions, such as substantially identical sectors.
12 . A method of producing space-qualified solar cells for a space-qualified solar cell assembly designed for operation at AM 0 and at a 1 MeV electron equivalent fluence of at least 5×10 14 e/cm 2 , comprising:
forming a III-V compound semiconductor multijunction solar cell including at least three subcells;
attaching a ceria doped borosilicate glass supporting member that is 3 to 6 mils in thickness to each space-qualified solar cell with a transparent adhesive;
forming a combination of compositions and band gaps of the space-qualified subcells designed to maximize efficiency of the space-qualified solar cell at a predetermined end-of-life (EOL) time period, after initial deployment when the space-qualified solar cell is deployed in space at AM 0 and at an operational temperature in the range of 40 to 70 degrees Centigrade, the EOL comprising at least five years; and
dividing at least one substantially circular space-qualified solar cell wafer into a plurality of portions, each portion being a space-qualified solar cell, at least some of the portions having at least one substantially straight edge and one substantially curved edge corresponding to an arc of the circumference of the space-qualified solar cell wafer.
13 . The method of claim 12 , wherein said portions are sectors of the circular space-qualified solar cell wafer.
14 . The method of claim 13 , wherein said sectors are quadrants of circles or are semicircles or both.
15 . A method of producing a space-qualified solar cell assembly, comprising the steps of providing a plurality of space-qualified solar cells with the method of claim 12 , and assembling said space-qualified solar cells to provide a substantially rectangular space-qualified solar cell assembly.
16 . The method of claim 15 , comprising the step of arranging the space-qualified solar cells according to a pattern of identical rectangular unit cells arranged in an array forming the substantially rectangular space-qualified solar cell assembly, each unit cell including an identical arrangement of at least two space-qualified solar cells.
17 . The method of claim 15 , wherein the space-qualified solar cells are substantially identical.