Abstract: A polymer matrix composite includes layers that alternate between a thin carbon fiber veil layer and a thicker base carbon fiber reinforcement layer. Each veil is coated with conductive carbon nanotubes (CNTs) prior to being added as a laminate layer. Epoxy resin fixes CNTs extended into adjacent reinforcement layers, which results in a composite improved in interlaminar strength, fracture toughness, and impact resistance. Thermal and electrical conductivity are also improved due to the conductive CNTs bridging the resin-insulating interlayer region. As the fuzzy fiber veil is not relied on to provide strength or stiffness to the composite structure, any damage to the veil will not affect composite integrity. Also, as the CNT growth is not on a replacement section of reinforcement layer, the composite avoids pitfalls of strength degradation, reinforcing phase continuity disruption, and residual stress introduction.

Abstract: Recycling devices for producing additive manufacturing filament from received materials including objects to be recycled, discarded objects, obsolete objects, and the like. A recycling device may include a material processing system an extrusion mechanism and a spooling assembly. The material processing system receives material, reduces the size of the received material via a material size reducer and actively pushes the material through at least a portion of the device. The extrusion mechanism produces filament from the material and the spooling assembly loads the filament onto a spool for later use. The spooling assembly may include detachable elements configured to interface with and supply filament to an additive manufacturing device. Depending on configuration, recycling devices may create filament from plastic, metal, in-situ material, or a combination thereof.

Abstract: A binder material activating device to activate a binder material on a fibrous substrate, the binder material activating device including a heat exposing device to expose the fibrous substrate with the binder material to heat. The heat exposing device includes a non-focused light source to provide a non-focused light beam and an optics device to be arranged in between the fibrous substrate to be exposed to heat and the light source to focus the non-focused light beam onto the fibrous substrate. Further, a preforming device includes the binder material activating device.

Abstract: A waveguide assembly for a radio frequency (RF) signal network can include a plurality of waveguides, wherein at least two of the plurality of waveguides are integrally formed with each other. A satellite payload can include the waveguide assembly, a method of manufacturing a waveguide assembly, and a method of manufacturing a signal network. Also provided is a waveguide connector having a flange, and a plurality of ports, wherein the flange can couple to a further waveguide connector, each port of the plurality of ports being configured to interface with a respective waveguide.

Abstract: A method of visibility event navigation includes receiving, via processing circuitry of a client device, a first visibility event packet from a server, the first visibility event packet including information representing 3D surface elements of an environmental model that are occluded from a first viewcell and not occluded from a second viewcell, the first and second viewcells representing spatial regions of a specified navigational route within a real environment modeled by the environmental model. The method also includes acquiring, surface information representing the visible surfaces of the real environment at a sensor and determining, a position in the real environment by matching the surface information to the visibility event packet information. The method further includes transmitting, the position from the client device to the server and receiving a second visibility event packet from the server if the at least one position is within the specified navigational route.

Abstract: An aircraft has a propulsion unit and a fuselage unit. The propulsion unit has a first rotor for providing a propulsion force on the aircraft. The fuselage unit extends along a rotation axis of the first rotor and has a rotationally symmetrical shape with respect to the rotation axis of the first rotor. The fuselage unit has a suspension at a first end by which the fuselage unit is coupled to the first rotor so that the fuselage unit is spaced apart from the first rotor along the rotation axis. A detection unit for the detection of environmental information is provided in the area of a second end of the fuselage unit. The propulsion unit is designed to keep the aircraft in a hovering flight condition so that a relative position of the aircraft with respect to a reference point on the Earth's surface remains unchanged.

Abstract: A system comprising an additive manufacturing device to create a macrostructure as a continuous piece, an applicator to apply a conductive coating to an inner surface of the macrostructure, and a signal attenuation tuner to attenuate a signal by modification of a physical dimension of the macrostructure. A method and another system are also disclosed.

Abstract: This disclosure provides water processing apparatuses, systems, and methods for recovering purified water and concentrated brine from wastewater. The water processing apparatuses, systems, and methods utilize ionomer membrane technology to separate water vapor from volatiles of a wastewater stream. The wastewater stream is evaporated into a gas stream including water vapor and volatiles of the wastewater stream in an evaporation container. The gas stream is delivered to a water separation module spatially separated from and fluidly coupled to the evaporation container. The water vapor of the gas stream is separated out in the water separation module while the volatiles are rejected. The water vapor can be collected into purified water while concentrated brine from the wastewater stream is left behind in the evaporation container.

Abstract: Technique for altering a client spacecraft's rotational rate including the precise positioning of a servicing spacecraft in close proximity of a client spacecraft, alignment of a fluid release output device on the servicing spacecraft that imparts a force on the client spacecraft by means of fluid release, and subsequent use of the fluid release output device to mitigate tumbling of the client spacecraft. This allows the servicing spacecraft to slow the rotation of a tumbling client spacecraft in order to perform additional servicing operations.

Abstract: An apparatus, including a light emitting device, including a plurality of sets of light emitting diodes, and further including a control device for controlling a light intensity of each light emitting diode of the plurality of sets of light emitting diodes is presented. Each set of the plurality of sets may be controlled by a driver. Each driver of each set of the plurality of sets may be configured to control an intensity of light emitted by each set of the plurality of sets. The control device may be programmed by a computer program to control light intensity of each set light emitting diodes of the plurality of sets of light emitting diodes based on light intensity requirements of vegetation that may be stored in the adjustment potentiometers or in the on-board computer memory via network connection or direct plugin modules.

Abstract: Disclosed herein is a double-reflector antenna (1) for use on board a satellite or space platform for data downlink or for telemetry, tracking and command. Said double-reflector antenna (1) comprises a main reflector (11) and a sub-reflector (12) arranged coaxially with, and in front of, one another. Additionally, the double-reflector antenna (1) further comprises a coaxial feeder, that is arranged coaxially with the main reflector (11) and the sub-reflector (12), and that includes inner (14) and outer (13) conductors arranged coaxially with, and spaced apart from, one another. The coaxial feeder is designed to be fed with downlink microwave signals to be transmitted by the double-reflector antenna (1), and to radiate said downlink microwave signals through a feed aperture (15), that is located centrally with respect to the main reflector (11) and that gives onto the sub-reflector (12).

Abstract: A method of controlling transmission of signals in a group of beams emitted by a satellite, wherein each beam has an associated area of coverage, includes adjusting an allocation of a channel resource by re-distributing portions of the channel resource among the beams in the group of beams in accordance with respective capacity demands for the areas of coverage of the beams in the group. The method further includes obtaining, for each of the areas of coverage, an indication of a signal quality from a terminal in the respective area of coverage for the adjusted allocation of the channel resource, and applying a co-channel interference mitigating technique to the group of beams in accordance with the obtained indications of the signal quality. The application further relates to an apparatus for performing such method.

Abstract: Systems and methods for satellite Synthetic Aperture Radar (SAR) artifact suppression for enhanced three-dimensional feature extraction, change detection, and/or visualizations are described. In some aspects, the described systems and methods include a method for suppressing artifacts from complex SAR data associated with a scene. In some aspects, the described systems and methods include a method for creating a photo-realistic 3D model of a scene based on complex SAR data associated with a scene. In some aspects, the described systems and methods include a method for identifying three-dimensional (3D) features and changes in SAR imagery.

Abstract: A product display merchandiser includes a tray having a top product-supporting surface with a longitudinally extending channel defined therein. A first sidewall has a vertical portion and a horizontal portion, and at least a laterally inner part of the horizontal portion can slide laterally with respect to the tray between a bottom of the tray and a base plate below the tray. A front end of the tray has a fitting received in a socket in the base plate. At a rear end of the tray, the channel receives a support assembly that connects the tray to a support structure.

Abstract: A product display merchandiser includes a tray having a product-supporting surface; a base plate situated below the tray; and a sidewall subassembly coupled to the tray and the base plate. The sidewall subassembly has a first sidewall adjacent a first lateral side of the tray and a second sidewall adjacent a second lateral side of the tray. Each of the first and second sidewalls has a vertical portion and a horizontally projecting tab. A portion of the horizontally projecting tab of the first sidewall slidably interfaces with a portion of the horizontally projecting tab of the second sidewall such that the vertical portions of the first and second sidewalls are laterally adjustable relative to one another and the base plate.

Abstract: In order to provide processor elements and programmable devices, which have little restriction on logical block arrangement and wiring, and which can improve a degree of integration, processor element 1 includes: arithmetic units 11 that perform arithmetic processing on the basis of functions which have implemented instruction sets generated in accordance with programs; registers 12 that store arguments of the functions; bypass switches 13 of the arithmetic units 11; bypass switches 14 of the registers 12; a connection setting unit 16 that switches the connections of function units 20; a multiplexer 17 that switches the input to the connection setting unit 16; a demultiplexer 18 that switches the output destination of the output from the connection setting unit 16; and a selection unit 15 that switches, in accordance with a state, the bypass switches 13, 14, the connection setting unit 16, the multiplexer 17 and the demultiplexer 18.

Abstract: A deployable mast structure (100) is disclosed, comprising a body configured to adopt a tubular shape when the mast structure is in a deployed configuration, and a plurality of openings (102) formed in a wall of the body so as to define a plurality of integral tape-spring hinges (103) in the wall of the body, the plurality of openings being configured so as to permit the body to collapse along its longitudinal axis into a stowed configuration when the tape-spring hinges are buckled. In the stowed configuration, the integral tape-spring hinges are configured to exert a force which urges the structure towards the deployed configuration. Since the mast structure collapses along its longitudinal axis, the structure only occupies a small volume in the stowed configuration. A method of fabricating the deployable mast structure from a layered composite material is also disclosed.

Abstract: An apparatus and method for creating shapes (e.g., letters, numbers, characters, symbols, or a combination thereof) using shape memory alloy (SMAs) component. The SMA components shaped into formed shapes that can then be distorted to obscure the original formed shaped. The original formed shape can be restored upon exposure to a heat source, magnetic field, or upon load removal.

Abstract: A spacecraft (10), comprising a body (12), a solar array (30) with a support panel (32) which is connected to the body, and a thermal radiator (50) that is connected to the body and which includes a radiator substrate (52) that is thermally coupled to the body via at least one heat link (64). The solar array and thermal radiator are configured to be transitioned from a stowed state wherein the support panel and the radiator substrate are held fixed in an overlapping arrangement along and near the body, to a deployed state wherein the solar array is unfolded with the support panel positioned at a distance from the body and the radiator substrate is folded away from the body and the solar array. Preferably, the solar array and thermal radiator are flexible, to allow them to be kept in an overlapping and temporarily bent shape in the stowed state.