Abstract: A high efficiency, light weight solar concentrator array particularly suitable for use with space vehicles. Parallel rows of mirror assemblies are mounted on a base plate having high thermal conductivity. Each mirror assembly comprises back-to-back mirror strips having reflecting front faces. Photovoltaic cells are placed ion the base plate between rows of mirror assemblies. The reflecting faces reflect incident light to the photovoltaic cells to produce electric power. Preferably, the reflecting faces have a cylindrical parabolic configuration with a line of focus approximately along the interface between the photovoltaic cell and the edge of the opposite mirror strip adjacent to the cell. The mirror strips may typically be roll formed from metal strips, cast from fiber reinforced plastic material and coated with a reflecting layers, etc.

Abstract: A self supporting solar concentrator cell array adapted for use in space applications that includes a plurality of cylindric parabolic reflective mirror surfaces, each of which focus recipient sunlight forwardly onto a focal line which is positioned approximately on the backside of an adjacent mirror surface on which is secured a solar element for converting the focussed sunlight into electricity. A front element extending upwardly from the leading edge of each mirror surface cooperates in providing an aperture through which the focussed sunlight passes and side elements close each cell element. The backside of each mirror is provided with a thermally emissive surface to provide mirror thermal control and allows the mirror to act as a thermal radiator fin for the solar cell elements. The mirror surface is provided with a highly reflective coating such as aluminum or silver to optimize reflectivity.

Abstract: An apparatus and method for providing a specified amount of heat on a test specimen, a portion of a specimen, or multiple specimens, under space-like conditions. This system includes a vacuum chamber in which one or more test specimens are placed. This chamber is evacuated to the necessary vacuum. One or more external sources of high intensity light is used for providing the necessary temperature. One or more reflectors are used for concentrating the high intensity light. A fiber optic light guide is used for receiving concentrated light from the reflector. A port in the vacuum chamber wall is used so that the second end of the light guide can extend into the chamber so that light exiting the second end impinges on a selected area of the test specimen. A positioning apparatus is used for locating the second end of the light guide within the housing adjacent to vary the test specimen area subjected to the light.

Abstract: A solar concentrator panel having an array of off axis cylindrical parabolic mirrors with an optical design of relatively short focal length solar cells arranged in line that converts sunlight to electricity. The back surface of the mirrors are used as the solar cell mount and the heat sink for the adjacent mirror.

Abstract: A deployable/retractable photovoltaic concentrator solar array assembly for space applications that includes a plurality of solar array panels that are carried by a pantograph arm arrangement that is deployable to position the panels in a predetermined canted arrangement for receipt of solar radiation. Each panel includes a plurality of spaced cylindrical off axis parabolic mirrors that concentrate the reflected light on a line that falls upon a series of photovoltaic cells arranged longitudinally along the back of each mirror. The cylindrical parabolic mirrors are aligned with the cylindrical axis perpendicular to the axis about which the panels are canted, so that such canting causes no loss of focus. The array panels may be hardened to resist perceived threats and the pantograph arm arrangement is operable to position the array panels in a preferred orientation according to the nature of the threat.

Abstract: A modular distributed concentrating collector using a low loss power bus to route solar radiation collected from a plurality of concentrating and collecting dishes to a centralized converted for conversion into electricity in space. The power bus may utilize fiber optic bundles. The collector includes a plurality of adjustable solar collectors to provide optimum tracking of the sun. The arrangement can be folded for stowing in the payload bay of the Space Shuttle or other launch vehicle for transport to a location in space.

Abstract: Inexpensive, highly efficient, flexible, fiber optic light guide which includes a plurality of flexible optic fibers which are unclad along their length and arranged in a bundle to increase packing density with all the ends of the fibers of the bundle falling in common planes at the entry and exit ends of the light guide. The flexible optic fiber bundle is provided with a suitable protective cladding which also may include a layer of clad optic fibers that surround the bundle. Light incident at one end of the light guide is reflected internally along the longitudinal length of the guide by a cladding boundary or space boundary so that transmission losses are minimized. Suitable ferrules may be provided at each end of the light guide.

Abstract: The solar simulator of the invention comprises a source of high intensity light simulating as closely as possible the spectral radiance of the sun directed through a flexible optic light guide into a chamber and pressure sealed through a chamber wall where this light is then directed on to a test specimen in a column or otherwise. The high intensity light is provided by one or more illuminating sources which can be positioned at the distal end or ends of the fiber optics or embedded within a fiber or liquid optic core.

Abstract: A point focus solar concentrator which uses various geometries of cylindrical reflector strips some of which are tilted to simulate a point focus by overlaying the line focii of each segment at a coincident point. Several embodiments of the invention are disclosed that use cylindrical parabolic, cylindrical hyperbolic or flat reflector strips to concentrate incident solar energy for use by a solar dynamic engine located at the focal point. Also disclosed is a combined photovoltaic/solar dynamic engine concentrator energy system that uses this arrangement of mirrors.

Abstract: A method of making a thin gallium arsenide solar cell having a reflecting back surface and coplanar electrical contacts. A photovoltaic cell comprising gallium arsenide is produced in a self-supporting thickness by conventional methods. A pattern of contact lines and a bus contact are formed on the front surface of the cell and a transparent coverslide is bonded thereover. The back of the cell is chemically etched away until the minimum effective thickness is reached, then etching in the bus contact region is continued until the bus is exposed. Any stop-etch material used to prevent excessive etching of the cell material is removed and a reflective contact material is applied to the back of the cell. The resulting solar cell is light in weight and both front and back connections can be made from the back of the cell, making it particularly suitable for use in space-based arrays.

Abstract: A solar energy splitting photovoltaic concentrator system that includes a first reflector that concentrates and directs sunlight to a high energy bandgap first photovoltaic array that absorbs and converts into electricity high energy photons. A second reflector formed integrally with the first photovoltaic array concentrates and reflects low energy photons back through the first photovoltaic array, which is transparent to the low energy photon, to a low energy bandgap second photovoltaic array that absorbs and converts the low energy photons.