Abstract: A multijunction solar cells that include one or more graded-index reflector structures disposed beneath a base layer of one or more solar subcells. The graded-index reflector structure is constructed such that (i) at least a portion of light of a first spectral wavelength range that enters and passes through a solar cell above the graded-index reflector structure is reflected back into the solar subcell by the graded-index reflector structure; and (ii) at least a portion of light of a second spectral wavelength range that enters and passes through the solar cell above the graded-index reflector structure is transmitted through the graded-index reflector structure to layers disposed beneath the graded-index reflector structure. The second spectral wavelength range is composed of greater wavelengths than the wavelengths of the first spectral wavelength range.

Abstract: The present disclosure provides interconnect elements and methods of using interconnect elements. In one embodiment, the interconnect element includes: a first end including at least three members, each member having a pair of parallel gap weld positions for mounting an adjoining first component; a second opposing end including at least two members, each member having a pair of parallel gap weld positions for mounting an adjoining second component; and one or more interconnect connecting portions to attach the first end of the interconnect element to the second end of the interconnect element.

Abstract: A multijunction solar cell includes an InGaAs buffer layer and an InGaAlAs grading interlayer disposed below, and adjacent to, the InGaAs buffer layer. The grading interlayer achieves a transition in lattice constant from one solar subcell to another solar subcell.

Abstract: A multijunction solar cell having an upper first solar subcell composed of a semiconductor material having a first band gap; a second solar subcell adjacent to said first solar subcell and composed of a semiconductor material having a second band gap smaller than the first band gap and being lattice matched with the upper first solar subcell; a third solar subcell adjacent to said second solar subcell and composed of a semiconductor material having a third band gap smaller than the second band gap and being lattice matched with the second solar subcell; a fourth solar subcell adjacent to and lattice mismatched from said third solar subcell and composed of germanium grown on a growth substrate. In some embodiments of a five junction solar cell, the growth substrate forms a bottom solar subcell and is composed of germanium.

Abstract: A method of manufacturing an inverted metamorphic multijunction solar cell is disclosed herein. The method includes forming a lattice constant transition material positioned between a first subcell and a second subcell using a metal organic chemical vapor deposition (MOCVD) reactor. The solar cell further includes at least one distributed Bragg reflector (DBR) layer directly adjacent a back surface field (BSF) layer.

Abstract: In one aspect, the present disclosure provides a power management system for a space vehicle, the system including: a photovoltaic array including a plurality of panels, wherein each panel includes one or more solar cell strings, each solar cell string including a plurality of photovoltaic cells connected in series to produce direct current (DC) power; at least one regulator module disposed on each of the one or more solar cell strings, the at least one regulator module being configured to condition the DC power produced by the one or more solar cell strings in the panel and supply it through at least one electrical connection line to the electrical power harness to route said power to a root power management unit; and an interface configured to transfer power produced by the photovoltaic array from the root power management unit to the vehicle, the interface having a first end configured to be connectable with the vehicle and a second end configured to be connectable with the photovoltaic array.

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 multijunction solar cell assembly and its method of manufacture including first and second discrete and different semiconductor body subassemblies which are electrically interconnected to form a five junction solar cell, each semiconductor body subassembly including first, second, third and fourth lattice matched subcells; wherein the average band gap of all four cells in each subassembly is greater than 1.44 eV.

Abstract: An airfoil body for an aircraft extending from an inner end to an outer end, between a leading edge and a trailing edge and having a pressure surface and a suction surface, the airfoil body having an outer surface and an inner support structure, the outer surface including a fixed skin section and a movable skin section, wherein the movable skin section comprises a first portion including an array of transducer elements, and the airfoil body including an actuator for moving the movable skin section to selectively position the transducer elements on the outer surface.

Abstract: The disclosure relates to an airfoil body for an aircraft extending from an inner end to an outer end, and between a leading edge and a trailing edge. The airfoil body comprises an internal structure and a skin covering the internal structure. The skin has a pressure side and a suction side, and the suction side includes a light transmitting portion. The internal structure includes an array of solar cells configured to receive solar light through the light transmitting portion. The present disclosure further relates to wings and aerial vehicles.

Abstract: A method of bonding solar cell component to a support and the solar cell assembly thus obtained. The method of bonding solar cell component to a support comprises: disposing metallized traces on the support; dispensing bonding adhesive on front of the support or on back of the solar cell component; and laying down the solar cell component on the support and soldering the solar cell component to the metallized traces on the support. The support is a glass support with integrated circuits.

Abstract: A vehicle such as an aircraft on which a solar cell assembly is mounted on a surface of the space vehicle. The solar cell assembly may be prepared on an assembly fixture. The solar cell assembly may then be removed from the assembly fixture and positioned on a top surface of the streamlined body of the vehicle. In examples, the solar cell assembly comprises a first film, an array of solar cells on top of the first film, and a second silicone film deposited over the solar cells.

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 multijunction solar cell assembly and its method of manufacture including first and second discrete and different semiconductor body subassemblies which are electrically interconnected to form a five junction solar cell, each semiconductor body subassembly including first, second, third and fourth lattice matched subcells; wherein the average band gap of all four cells in each subassembly is greater than 1.44 eV.

Abstract: A flexible solar cell assembly and methods for its manufacture are described. The flexible solar cell assembly comprises: solar cells comprising opposing top and back surfaces of different polarities, a contact at the top surface and a contact at the back surface; a flexible substrate; and conductive traces having end portions bonded to the top and bottom contacts of different solar cells so as to interconnect them in electrical series.