Abstract:
A solar battery having a board with a surface with a plurality of spherical segments projecting from the board surface. A primary electrode layer is provided on the board surface and the plurality of spherical segments. A semiconductor layer is provided on the primary electrode layer and has P-N connecting members. A secondary electrode layer on the semiconductor layer is made up of a translucent material.
Abstract:
A radiation tolerant solar cell array module which can be efficiently assembled into a larger solar panel to generate power for a spacecraft the module includes at least first and second single-crystal solar cells. The first and second solar cells have front sides and back sides. At least one of the solar cells has a shallow junction N on P structure. A first contact is formed on at least the back side of the first solar cell. A second contact formed on at least the back side of the second solar cell. A conductor is in electrical communication with the first contact and the second contact. A substantially transparent ceria-doped cover overlays at least a portion of each of the solar cells. The cover remains substantially transparent when exposed to an AM0 space radiation environment. A substantially transparent adhesive is situated between the cover and the solar cell portions. The adhesive remains substantially transparent when exposed to a space radiation environment.
Abstract:
A multilayer semiconductor structure includes a germanium substrate having a first surface. The germanium substrate has two regions, a bulk p-type germanium region, and a phosphorus-doped n-type germanium region adjacent to the first surface. A layer of a phosphide material overlies and contacts the first surface of the germanium substrate. A layer of gallium arsenide overlies and contacts the layer of the phosphide material, and electrical contacts may be added to form a solar cell. Additional photovoltaic junctions may be added to form multijunction solar cells. The solar cells may be assembled together to form solar panels.
Abstract:
A charging control device for use with a spacecraft solar array employs a field emitter array including a cathode and an anode; a first resistor coupled between the cathode of the field emitter array and a solar array common; and a second resistor coupled between the anode of the field emitter array and a solar array positive.
Abstract:
A power generation satellite has a photoelectric conversion unit for converting sunlight into electric energy, a transmission frequency conversion unit for performing frequency conversion of the electric energy to a microwave, a microwave control unit for controlling the amplitude, the phase, or the amplitude and the phase of the microwave, and a transmitting antenna for radiating the microwave. A plurality of the power generation satellites are placed in space to form a power generation satellite group and an array antenna having the transmitting antennas of the power generation satellites in the power generation satellite group as element antennas is formed.
Abstract:
A solar cell module includes an electrical parameter detection unit including an operating current detector unit for a solar cell element and a communication unit for communicating an output from the operating current detection unit, thereby providing a solar cell module capable of easily specifying a malfunctioning solar cell module.
Abstract:
A space photovoltaic generation system including a plurality of power satellites arranged in space, each of which converts electrical energy, into which sunlight has been photoelectric-converted, into a microwave, and transmits the microwave to an electric power base. The system can thus transmit a microwave of high power to the electric power base. Each of the plurality of power satellites modulates the generated microwave so as to generate an incoherent microwave before transmitting it to the electric power base, thus reducing the power density of the electric power transmitted to the electric power base on the earth and hence a loss in the total amount of energy transmitted to the electrical power base on the earth.
Abstract:
A solar system for a motor vehicle, which is provided with a solar generator and a DC/DC converter unit, the solar system being switchable for supplying a power consuming device in the motor vehicle or for recharging of the motor vehicle battery. The DC/DC converter unit is made with two poles on the output side and functionally comprises a first and a second DC/DC converter which are respectively optimized with respect to the supply function of the power consuming device and the recharging function, there being a changeover unit which acquires the voltage at the output of the DC/DC converter unit and switches the output depending on the acquired voltage to either the first DC/DC converter or the second DC/DC converter.
Abstract:
A device, having circuits formed thereon, comprises a circuit including a frequency generator for generating a detectable radio frequency energy when powered and a power generator, coupled to the frequency generator, for generating power when exposed to light.
Abstract:
Disclosed is a photovoltaic device comprising on a substrate (1) a plurality of photovoltaic elements (10) each composed of a lamination body of a first electrode (2), a photovoltaic conversion layer (3), and a second electrode (4), the thickness of a side end (B) in the first electrode (2) in the vicinity of a separating trench (S) existing between the first electrode (2) and the adjacent first electrode (2) being larger than the thickness of an element region (A) in the first electrode (2).