Embodiments of the disclosure a reflective frame of a multicell solar panel to reduce radiant heating on a surface of the solar panel. According to one embodiment, a solar panel mask can comprise a reflective layer comprising a planar sheet of light reflective material and a plurality of cutouts in the reflective layer positioned to expose each of a plurality of solar cells of a solar panel to an incident light source when the solar panel mask is positioned on the solar panel. The plurality of cutouts can form the reflective layer into a reflective frame.

Embodiments of the disclosure a reflective frame of a multicell solar panel to reduce radiant heating on a surface of the solar panel. According to one embodiment, a solar panel mask can comprise a reflective layer comprising a planar sheet of light reflective material and a plurality of cutouts in the reflective layer positioned to expose each of a plurality of solar cells of a solar panel to an incident light source when the solar panel mask is positioned on the solar panel. The plurality of cutouts can form the reflective layer into a reflective frame.

A system and method are disclosed for internally heated concentrated solar power (CSP) thermal absorbers. The system and method involve an energy-generating device having at least one heating unit. At least one heating unit preheats the energy-generating device in order to expedite the startup time of the energy-generating device, thereby allowing for an increase in efficiency for the production of energy. In some embodiments, the energy-generating device is a CSP thermal absorber. The CSP thermal absorber comprises a housing, a thermal barrier, a light-transparent reservoir containing a liquid alkali metal, at least one alkali metal thermal-to-electric converter (AMTEC) cell, an artery return channel, and at least one heating unit. Each heating unit comprises a heating device and a metal fin. The metal fin is submerged into the liquid alkali metal, thereby allowing the heating device to heat the liquid alkali metal via the fin.

A system and method are disclosed for internally heated concentrated solar power (CSP) thermal absorbers. The system and method involve an energy-generating device having at least one heating unit. At least one heating unit preheats the energy-generating device in order to expedite the startup time of the energy-generating device, thereby allowing for an increase in efficiency for the production of energy. In some embodiments, the energy-generating device is a CSP thermal absorber. The CSP thermal absorber comprises a housing, a thermal barrier, a light-transparent reservoir containing a liquid alkali metal, at least one alkali metal thermal-to-electric converter (AMTEC) cell, an artery return channel, and at least one heating unit. Each heating unit comprises a heating device and a metal fin. The metal fin is submerged into the liquid alkali metal, thereby allowing the heating device to heat the liquid alkali metal via the fin.

An apparatus comprises a plurality of power sources, one or more processors embedded with the plurality of power sources, and memory storing processor executable instructions that, when executed by the one or more processors, cause the apparatus to modify duty cycles of the power sources, and to modify timing for each phase of a multiphase cycle. In some cases, the apparatus: transfers, for each phase of the multiphase cycle, power from a different power source of a plurality of power sources to a load; determines, for each phase of the multiphase cycle, an input voltage associated with the transferred power, an output voltage associated with the transferred power, and current from the power source associated with the transferred power; determines a duty cycle associated with the power source; modifies duty cycles of the power sources; and modifies timing for each phase of the multiphase cycle.

Systems and methods are disclosed for intelligent circuit control for solar panel systems. In one embodiment, an example method may include determining, by a controller, that a first electrical output of a first solar panel configured to charge a plurality of rechargeable batteries is greater than a second electrical output of a second solar panel configured to charge the plurality of rechargeable batteries, and causing the second solar panel to be disconnected from the plurality of rechargeable batteries. Example methods may include determining that a voltage potential of the plurality of rechargeable batteries is greater than a total output voltage, where the total output voltage is a sum of the first electrical output and the second electrical output, and causing a connection between the plurality of rechargeable batteries to be changed from a series connection to a parallel connection based at least in part on the first electrical output.

Systems and methods are disclosed for intelligent circuit control for solar panel systems. In one embodiment, an example method may include determining, by a controller, that a first electrical output of a first solar panel configured to charge a plurality of rechargeable batteries is greater than a second electrical output of a second solar panel configured to charge the plurality of rechargeable batteries, and causing the second solar panel to be disconnected from the plurality of rechargeable batteries. Example methods may include determining that a voltage potential of the plurality of rechargeable batteries is greater than a total output voltage, where the total output voltage is a sum of the first electrical output and the second electrical output, and causing a connection between the plurality of rechargeable batteries to be changed from a series connection to a parallel connection based at least in part on the first electrical output.

A space system including a layered structure on an outer surface of the space system, the layered structure including a conductive veil or nonwoven comprising conductive fibers, and a non-conductive sheet arranged on a surface of the conductive veil or nonwoven.

A space system including a layered structure on an outer surface of the space system, the layered structure including a conductive veil or nonwoven comprising conductive fibers, and a non-conductive sheet arranged on a surface of the conductive veil or nonwoven.

Deployable solar panels are disclosed. In some embodiments, the deployable solar panel includes an extendable member comprising a composite material and having a length and a width; a plurality of hinges, each of the plurality of hinges extending across the width of the extendable member, the plurality of hinges comprising composite material and a shape memory polymer; and a plurality of solar panels coupled with the extendable member. In some embodiments, the deployable solar panel includes a lenticular shape extending along the length of the extendable member.