Abstract: A product display merchandiser comprising a tray, a spring biased pusher slidable within the tray, and a visual indicator comprising at least one light activated by a switch, the switch configured to be actuated when the pusher is within a predetermined portion of the tray.

Abstract: A solar cell stack, having a first semiconductor solar cell having a p-n junction made of a first material with a first lattice constant, and a second semiconductor solar cell having a p-n junction made of a second material with a second lattice constant, and the first lattice constant being at least 0.008 ? smaller than the second lattice constant, and a metamorphic buffer, the metamorphic buffer being formed between the first semiconductor solar cell and the second semiconductor solar cell, and the metamorphic buffer including a series of three layers, and the lattice constant increasing in a series in the direction of the semiconductor solar cell, and the lattice constants of the layers of the metamorphic buffer being bigger than the first lattice constant, two layers of the buffer having a doping, and the difference in the dopant concentration between the two layers being greater than 4E17 cm?3.

Abstract: To provide a technology in which a differential phase modulation manner can be applied to a space environment for satellite mounting, the optical receiver 10 includes a digital signal processing unit has: a level fluctuation frequency suppression unit 320 which suppresses a level fluctuation frequency component of the peak signal; an optical delay interference control unit 330 which generates an optical delay interference control signal, which is overdrive-amplified, on the basis of the peak signal of which the level fluctuation frequency component is suppressed and applies the generated optical delay interference control signal to the optical delay interferometer 210; and a data recovery unit 310 which recovers output data on the basis of the main signal from the wideband balanced optical detector 240.

Abstract: A satellite includes a plurality of thrusters disposed about the satellite, each of the plurality of thrusters having a minimum thruster firing time, and a control circuit connected to the plurality of thrusters. The control circuit is configured to identify violations of the minimum thruster firing time in a non-compliant thruster firing pattern selected to achieve a specified movement, generate a plurality of compliant thruster firing patterns by replacing each of the violations of the non-compliant thruster firing pattern by zero and a minimum time in different combinations, select a compliant thruster firing pattern from the plurality of compliant thruster firing patterns to produce a satellite movement that is within a predetermined range of the specified movement, and cause the plurality of thrusters to fire according to the compliant thruster firing pattern.

Abstract: A synchronization device and a synchronization method for synchronizing a first node and a second node are provided. The first node supports a first time protocol profile, and the second node supports a second time protocol profile. The synchronization method includes: providing a system operating time by a counter; communicating with the first node based on the first time protocol profile to obtain first synchronization information; calculating a time delay according to the first synchronization information, and correcting the system operating time according to the time delay to generate a corrected system operating time; and communicating with the second node based on the second time protocol profile so as to provide the second node with second synchronization information according to the corrected system operating time.

Abstract: A spacecraft includes a structural interface adapter for mating to a launch vehicle, at least one radiator panel, at least one equipment panel, a first 3-D truss structure proximal to and mechanically coupled with the structural interface adapter, and a second 3-D truss structure distal from the structural interface adapter and coupled mechanically with the structural interface adapter by way of the first 3-D truss structure. The at least one equipment panel and the at least one exterior radiator panel is coupled mechanically by one or both of the first 3-D truss structure and the second 3-D truss structure with the structural interface adapter. Each 3-D truss structure includes at least four coupling nodes and at least six strut elements, attached together by a respective plurality of joints, each strut element disposed between and attached with a respective pair of the plurality of coupling nodes.

Abstract: Methods of collecting in-situ materials on a celestial body for return to Earth or another location and associated devices are described. These devices and methods facilitate collection of samples and creation of portions of the return spacecraft via an additive manufacturing device contained within the lander craft. The additive manufacturing device is configured to produce portions of the return spacecraft (e.g., sample return container, spacecraft structure, heat shield) and may also be configured to place samples within the spacecraft for return and analysis.

Abstract: A system for transferring a fluid from a first spacecraft to a second spacecraft. The first spacecraft includes a fluid transfer system comprising: a pressurant supply system, a first fluid tank to store a fluid to be transferred, one or more transfer feedlines to provide fluidic connection between the first fluid tank and the second spacecraft, a connector for connecting the first spacecraft to the second spacecraft, an accumulator tank comprising a first portion connected to the pressurant supply system, a second portion configured in fluidic communication with the one or more transfer feedlines, and a flexible separator to separate the first portion and the second portion. The pressurant supply system supplies pressurant gas to the first fluid tank for pressurising the first fluid tank and to supply pressurant gas to the first portion of the accumulator tank for pressurising the first portion of the accumulator tank.

Abstract: A power transmission apparatus includes a controller that controls a power transmitter that performs wireless power transmission. The controller is configured to: cause the processor to: cause the power transmitter to emit a first power transmission beam for which a first power is set; acquire feedback information on a result of reception of the first power transmission beam in a power reception apparatus; identify a power receiving capability in the power reception apparatus; and determine, with reference to the power receiving capability and the reception result, a second power which is usable in wireless power supply for the power reception apparatus and which is larger than the first power. The power receiving capability includes a maximum value of an input power range of the power reception apparatus. The wireless power transmission uses an electromagnetic wave having a frequency equal to or higher than that of a microwave.

Abstract: A vapor phase epitaxy method including: providing a III-V substrate of a first conductivity type, introducing the III-V substrate into a reaction chamber of a vapor phase epitaxy system at a loading temperature, heating the III-V substrate from the loading temperature to an epitaxy temperature while introducing an initial gas flow, depositing a III-V layer with a dopant concentration of a dopant of the first conductivity type on a surface of the III-V substrate from the vapor phase from an epitaxial gas flow, fed into the reaction chamber and comprising the carrier gas, the first precursor, and at least one second precursor for an element of main group III, wherein during the heating from the loading temperature to the epitaxy temperature, a third precursor for a dopant of the first conductivity type is added to the initial gas flow.

Abstract: A wireless communications system includes a stochastic pre-distortion actuator configured to receive a carrier-modulated signal and convert the carrier-modulated signal into an output signal. The system includes one or more antennas configured to receive the output signal and transmit the output signal, one or more power amplifiers electrically coupled between the pre-distortion actuator and the one or more antennas and a receiver configured to receive the output signal over-the-air and generate feedback based on the output signal. The pre-distortion actuator is configured to generate the output signal by applying a correction to the carrier-modulated signal that cancels out nonlinearities associated with the one or more antennas and/or the one or more power amplifiers. The pre-distortion actuator is configured based on the feedback.

Abstract: An apparatus and a method of use are disclosed herein. The apparatus comprises a disaggregated fault tolerant backplane having a front side and a back side with at least two daughter card slots configured on the front side and configured to receive slot fanout signals over the backplane. The apparatus further comprises at least two switch boards (SBs) configured to provide electrical power to the at least two daughter card slots and at least one main fanout board (MFB) configured to send and receive SB control signals to and from the at least two SBs. The at least one MFB connects to the backplane through at least one MFB connector configured on the back side of the backplane. In one embodiment, the MFB receives control signals from the daughter card slots and sends slot fanout signals to the daughter card slots.

Abstract: A universal external port is proposed to add new functionality to or replace existing functionality of an already deployed spacecraft (e.g., a satellite in orbit). The universal external port is mounted on an external surface of the spacecraft and configured to connect to different types of external modules that have different functions, without removing components from the spacecraft other than one or more components of the universal external port. A communication interface onboard the spacecraft is configured to wirelessly receive a software patch from an entity remote from the spacecraft (e.g., from a ground terminal or other spacecraft) to program the spacecraft to change operation of the spacecraft to utilize the external module when the external module is connected to the universal external port.

Abstract: Enclosures for facilitating activities in space, and associated systems and methods, are disclosed. A representative system includes a spacecraft having an enclosed interior volume (which can be formed by an inflatable membrane) and one or more unmanned aerial vehicles (UAVs) carried by the spacecraft and positioned to deploy into the enclosed interior volume. The system can include a remote-control system to control the one or more UAVs from a terrestrial location while the spacecraft is in space. A wireless charging system can provide electrical power to the one or more UAVs. A representative method includes configuring one or more controllers to launch a first spacecraft to a first orbit, launch a second spacecraft to a second orbit, move the first spacecraft to the second orbit, dock the first spacecraft with the second spacecraft, and broadcast an event within an interior volume of the first spacecraft to a terrestrial location.

Abstract: A stacked monolithic multi-junction solar cell having at least four subcells, wherein the band gap increases starting from the first subcell in the direction of the fourth subcell, each subcell has an n-doped emitter and a p-doped base, the emitter and the base of the first subcell each are formed of germanium, all following subcells each have at least one element of main group III and V of the periodic table, all subcells following the first subcell are formed lattice-matched to one another, a semiconductor mirror having a plurality of doped semiconductor layers with alternately different refractive indices is placed between the first and second subcell, the semiconductor layers of the semiconductor mirror are each formed n-doped and each have a dopant concentration of at most 5·1018 cm?3, the semiconductor mirror is placed between the first subcell and the first tunnel diode.

Abstract: A stacked monolithic multi-junction solar cell having at least four subcells, wherein the band gap increases starting from the first subcell in the direction of the fourth subcell, each subcell has an n-doped emitter and a p-doped base, the emitter and the base of the first subcell each have germanium or consist of germanium, all following subcells each have at least one element of main group III and V of the periodic table, a tunnel diode with a p-n junction is placed between each two subcells, all subcells following the first subcell are formed lattice-matched to one another, a semiconductor mirror having a plurality of doped semiconductor layers with alternately different refractive indices is placed between the first and second subcell, and the semiconductor mirror is placed between the first subcell and the first tunnel diode.

Abstract: A firing simulation scope, for installation on a rifle, includes an inertial measurement unit, a windage correction adjustment device, an electronic system, a microphone, a display and an interface for connection to a control station.

Abstract: Methods aiding in proving shuffles of re-encryptions of ciphertexts and a mixnet employing such methods. A method for compacting ciphertexts includes encrypting a plaintext using an asymmetric key encryption scheme for a ciphertext, dividing the ciphertext into partial ciphertexts, encrypting each of the partial ciphertexts using the asymmetric key encryption scheme to obtain re-encrypted partial ciphertexts, creating hash exponents from a digest of a cryptographic hash function taking the partial ciphertexts, the re-encrypted partial ciphertexts and arbitrary salt values as argument of the cryptographic hash function, calculating a compacted ciphertext by multiplying all of the partial ciphertexts exponentiated by a respective one of the plurality of hash exponents, and calculating a compacted re-encrypted ciphertext by multiplying all of the re-encrypted partial ciphertexts exponentiated by a respective one of the hash exponents.

Abstract: A computer implemented method for detecting a set of relevant communities of accounts, the accounts being connected by at least one communication platform, includes collecting data from a stream of messages circulating on at least one communication platform; extracting interaction data and shared objects, the shared objects being shared among the accounts; processing each collected message in order to obtain content metadata; processing collected data in order to obtain an account profile of each account; from collected data building shared objects graphs and interaction graphs; building a resulting graph; applying a community detection method to the resulting graph to obtain a set of communities of accounts; computing quality indicators of the set of communities to obtain at least one score for each community the score enabling the selection of at least a relevant community.