Abstract: The disclosure relates to a metallic interconnect member for connecting a first solar cell to a second solar cell. The interconnect member includes one or more serpentine paths having substantially perpendicular loops. The interconnect member may include two connection pads for connecting to the first solar cell. A further connection pad for connecting to a bypass diode may be included. The disclosure further relates to a string of solar cells including a first and a second solar cell connected by an interconnect member.

Abstract: The disclosure relates to a metallic interconnect member for connecting a first solar cell to a second solar cell. The interconnect member includes one or more serpentine paths having substantially perpendicular loops. The interconnect member may include two connection pads for connecting to the first solar cell. A further connection pad for connecting to a bypass diode may be included. The disclosure further relates to a string of solar cells including a first and a second solar cell connected by an interconnect member.

Abstract: The disclosure relates to a metallic interconnect member for connecting a first solar cell to a second solar cell. The interconnect member includes one or more serpentine paths having substantially perpendicular loops. The interconnect member may include two connection pads for connecting to the first solar cell. A further connection pad for connecting to a bypass diode may be included. The disclosure further relates to a string of solar cells including a first and a second solar cell connected by an interconnect member.

Abstract: A flexible solar array for a spacecraft or aviation craft including a flexible backing substrate with conductive trace(s) formed thereon; solar cell subassemblies disposed over the flexible backing substrate, each of the solar cell subassemblies at least including a solar cell; and an adhesive layer interposed between the solar cell subassemblies and the flexible backing substrate, with the solar cell attached to the flexible backing substrate. The adhesive layer includes openings for exposing the corresponding conductive traces so that the exposed metal traces are adaptable to interconnect the solar cells of the respective adjacent solar cell subassemblies through the openings.

Abstract: A flexible solar array and a method for fabricating the same is provided. The flexible solar array may include a flexible backing substrate with conductive trace(s) formed thereon; solar cell subassemblies over the flexible backing substrate, each of the solar cell subassemblies at least including a solar cell; and an adhesive layer interposed between the solar cell subassemblies and the flexible backing substrate, and attaching the solar cells to the flexible backing substrate. The adhesive layer includes openings for exposing the corresponding conductive traces so that the exposed metal traces are adaptable to interconnect the solar cells of the respective adjacent solar cell subassemblies through the openings.

Abstract: The present disclosure provides a solar cell array for deployment and use in a space environment, and methods of making same. The array includes a plurality of solar cells having an emissivity coating on the baskside of each, with each coated solar cell being attached to a supporting member.