Abstract: A counter-swarm firework includes a shell casing, multiple streamers positioned in the shell casing, a burst charge positioned in the shell casing and configured to disperse the multiple streamers from the shell casing when discharged, a pusher plate positioned in the shell casing between the burst charge and the multiple streamers, a fire suppressant layer positioned between the burst charge and the pusher plate, and a kick charge configured to launch the shell casing and its contents prior to discharging the burst charge. The fire suppression layer may be configured to suppress heat generated by the discharge of the burst charge.

Abstract: A counter-swarm firework includes a shell casing, multiple streamers positioned in the shell casing, a burst charge positioned in the shell casing and configured to disperse the multiple streamers from the shell casing when discharged, a pusher plate positioned in the shell casing between the burst charge and the multiple streamers, a fire suppressant layer positioned between the burst charge and the pusher plate, and a kick charge configured to launch the shell casing and its contents prior to discharging the burst charge. The fire suppression layer may be configured to suppress heat generated by the discharge of the burst charge.

Abstract: For model predictive control for a spacecraft formation, a method calculates a virtual point that represents a plurality of spacecraft orbiting in a spacecraft formation. The method calculates an outer polytope boundary and an inner polytope boundary relative to the virtual point for a given spacecraft of the plurality of spacecraft. The method maneuvers the given spacecraft to within the inner polytope boundary using model predictive control (MPC) to minimize fuel consumption.

Abstract: For model predictive control for a spacecraft formation, a method calculates a virtual point that represents a plurality of spacecraft orbiting in a spacecraft formation. The method calculates an outer polytope boundary and an inner polytope boundary relative to the virtual point for a given spacecraft of the plurality of spacecraft. The method maneuvers the given spacecraft to within the inner polytope boundary using model predictive control (MPC) to minimize fuel consumption.

Abstract: For determining a communication window is disclosed, a method generates a communication graph that includes backbone nodes, dummy nodes, data collection nodes, downlink nodes, crosslink send nodes, and crosslink receive nodes. The backbone nodes, the data collection nodes, the downlink nodes, the crosslink-transmit nodes, and the crosslink-receive nodes are connected by one of a homogenous edge between nodes of a same type and transition edges between nodes of a different type. The method determines access windows for downlink communications and crosslink communications using the communication graph. The method selects access windows based on a task graph generated from the communication graph. The method communicates from a given satellite within the selected access windows.

Abstract: An interferometer includes a coherent light source and an array of electrically coupled light-sensitive pixel elements. The interferometer is configured to direct an internal optical path of the coherent light source and an external optical path of the coherent light source into a monolithic unit cell. In addition, the monolithic unit cell is configured to direct the internal optical path first through the monolithic unit cell and then onto the array and also configured to direct the external optical path back outside the monolithic unit cell through an external environment and then back into the monolithic unit cell and finally onto the array. In addition, interferometer is further configured to combine the internal optical path and the external optical path at the array and produce a first interferogram on the array, the interferogram characterizing an optical property of the external environment.

Abstract: A uniaxial optical multi-measurement imaging system includes an imaging lens column having an optical axis and configured to receive light from a scene from a single viewpoint. The imaging system also includes a light redistribution optic (LRO) in the shape of a thin pyramid shell with an apex. The LRO is centered along the optical axis with the apex pointing towards the imaging lens column. The LRO has planar sides with each side angled 45 degrees with respect to the optical axis and configured to reflect and transmit the light. The imaging system also includes a circumferential filter array (CFA) concentrically located around the LRO. The CFA is configured to filter the light reflected from or transmitted through the LRO. The imaging system includes multiple image sensors, each positioned to receive the light reflected from or transmitted through the LRO.

Abstract: In embodiments, a uniaxial optical multi-measurement sensor comprises a sensor housing having a center axis and a cylindrical surface and an array of electrically coupled light-sensitive pixel elements attached to the cylindrical surface. Each pixel element is positioned having its light-sensitive side facing towards the center axis. In this embodiment, a conical light redistribution optic is positioned along the center axis to direct or reimage uncollimated light entering the sensor housing onto the pixel elements. Also, in this embodiment, the pixel elements are positioned relative to the light redistribution optic to measure or image two or more properties of the uncollimated light entering the sensor housing of a single scene and from a single viewpoint.

Abstract: An aperture stop exploitation camera comprises an imaging lens column positioned along an optical axis and configured to transmit light from a scene from a single viewpoint and converge the light as it passes through the aperture stop. Also, the camera comprises a light redistribution optic (LRO) that is a thin V-shape having an apex. The LRO is centered along the optical axis with the apex pointing towards the imaging lens column. The LRO has two planar sides with each side angled 45 degrees with respect to the optical axis and each side configured to reflect and transmit the light transmitted from the imaging lens column into three independent, spatially separate images, each retaining all the spectral, polarimetric, and relative intensity information of the light from the scene. The camera comprises three image sensors, each image sensor positioned to receive one of the three independent, spatially separate images.

Abstract: For generating a points-of-interest plan, a method generates communication graph nodes for at least one satellite. The method calculates communication graph edges from the communication graph nodes, wherein the communication graph nodes and the communication graph edges comprise a communication graph. The method solves the communication graph to yield a communication plan. The method generates a points-of-interest plan from the communication plan.

Abstract: A counter-swarm firework includes a shell casing, multiple streamers positioned in the shell casing, a burst charge positioned in the shell casing and configured to disperse the multiple streamers from the shell casing when discharged, a pusher plate positioned in the shell casing between the burst charge and the multiple streamers, a fire suppressant layer positioned between the burst charge and the pusher plate, and a kick charge configured to launch the shell casing and its contents prior to discharging the burst charge. The fire suppression layer may be configured to suppress heat generated by the discharge of the burst charge.

Abstract: A hybrid propulsion system includes a housing, at least two electrodes, a solid-grain fuel material, a combustion chamber, an oxidizer port, and a nozzle. The housing has a first end and a second end and defines a cavity. The electrodes extend into the cavity. The fuel material is free of an oxidizer and is positioned in the cavity. The fuel material has a combustion surface and is exposed to the electrodes. The combustion chamber is defined between the combustion surface and the second end. The oxidizer port provides a flow of oxidizer to the combustion chamber. The nozzle is positioned at the second end. Combustion of the fuel material in the combustion chamber may be dominated by radiative heat transfer. Combustion of the fuel material in the combustion chamber may generate thrust of no more than 5 N at an oxidizer flow rate of no more than 5 g/s.

Abstract: A hybrid propulsion system includes a housing, at least two electrodes, a solid-grain fuel material, a combustion chamber, an oxidizer port, and a nozzle. The housing has a first end and a second end and defines a cavity. The electrodes extend into the cavity. The fuel material is free of an oxidizer and is positioned in the cavity. The fuel material has a combustion surface and is exposed to the electrodes. The combustion chamber is defined between the combustion surface and the second end. The oxidizer port provides a flow of oxidizer to the combustion chamber. The nozzle is positioned at the second end. Combustion of the fuel material in the combustion chamber may be dominated by radiative heat transfer.

Abstract: A hybrid propulsion system includes a housing, at least two electrodes, a solid-grain fuel material, a combustion chamber, an oxidizer port, and a nozzle. The housing has a first end and a second end and defines a cavity. The electrodes extend into the cavity. The fuel material is free of an oxidizer and is positioned in the cavity. The fuel material has a combustion surface and is exposed to the electrodes. The combustion chamber is defined between the combustion surface and the second end. The oxidizer port provides a flow of oxidizer to the combustion chamber. The nozzle is positioned at the second end. Combustion of the fuel material in the combustion chamber may be dominated by radiative heat transfer. Combustion of the fuel material in the combustion chamber may generate thrust of no more than 5 N at an oxidizer flow rate of no more than 5 g/s.

Abstract: Methods, systems, and devices for object detection are described. An example method for object detection is provided which may include capturing at least three polarization angles of a scene. The method may include translating polarization parameters associated with the at least three polarization angles to a reference angle to create a vector map and resolving the vector map into parallel components and perpendicular components, wherein the parallel components are parallel to a plane of incidence of light in the scene and the perpendicular components are perpendicular. The method may further include determining a range map based at least in part on the parallel and perpendicular components, detecting an object present in the scene using the range map and an airlight scattering polarization component, and outputting an indication of the object.

Abstract: Methods, systems, and devices for wireless communications are described. An example method for object detection is provided which may include capturing at least three polarization angles of a scene. The method may include translating polarization parameters associated with the at least three polarization angles to a reference angle to create a vector map and resolving the vector map into parallel components and perpendicular components, wherein the parallel components are parallel to a plane of incidence of light in the scene and the perpendicular components are perpendicular. The method may further include determining a range map based at least in part on the parallel and perpendicular components, detecting an object present in the scene using the range map and an airlight scattering polarization component, and outputting an indication of the object.

Abstract: A system includes a vacuum chamber to receive a laser beam and a charged nanoparticle. The nanoparticle oscillates at a trapping frequency in a focus of the laser beam. Resonant oscillation of the nanoparticle is driven by a presence of an ambient electric field adjacent to the vacuum chamber. The system also includes a controller to tune the trapping frequency of an oscillating nanoparticle to be in resonance with the ambient electric field causing on-resonant enhancement of the system; a detector to detect positional changes of the oscillating nanoparticle; and a processor to calculate an electromagnetic force of the ambient electric field based on the positional changes of the oscillating nanoparticle.

Abstract: A hybrid propulsion system includes a housing, at least two electrodes, a solid-grain fuel material, a combustion chamber, an oxidizer port, and a nozzle. The housing has a first end and a second end and defines a cavity. The electrodes extend into the cavity. The fuel material is free of an oxidizer and is positioned in the cavity. The fuel material has a combustion surface and is exposed to the electrodes. The combustion chamber is defined between the combustion surface and the second end. The oxidizer port provides a flow of oxidizer to the combustion chamber. The nozzle is positioned at the second end. Combustion of the fuel material in the combustion chamber may be dominated by radiative heat transfer. Combustion of the fuel material in the combustion chamber may generate thrust of no more than 5 N at an oxidizer flow rate of no more than 5 g/s.

Abstract: For measuring an area of interest based on a sensor task and/or routing sensor data, a method discovers a network topology for a network comprising a plurality of network nodes connected by links. The method dynamically generates a minimum spanning tree from the network topology. Given sensor data traverses one link of the minimum spanning tree only once. The method routes a sensor task to a sensor with a sensor motion track that includes an area of interest. The method measures the area of interest with the sensor based on the sensor task. The method routes sensor data from the measurement of the area of interest via links of the minimum spanning tree.

Abstract: A composite thermal strap includes a pyrolytic graphite stack with multiple pyrolytic graphite sheets and first and second metal foils immediately adjacent and in thermal contact with the top and bottom faces of the pyrolytic graphite stack, together forming a composite stack. The first and second metal foils do not envelop the front and back sides of the pyrolytic graphite stack. A composite thermal strap also includes first and second metal end blocks with inside surfaces connected to and thermally linked to either end of the composite stack. Also disclosed is a particle containment sleeve configured to capture pyrolytic graphite particles or metal particles that may rub off from the composite stack. Also disclosed is a snorkel, configured to pass air from within a volume encapsulated by the particle containment sleeve and the atmosphere.