Abstract: Systems and methods for providing a solar cell array with a reduced magnetic field are provided. The systems include a plurality of solar cells arrayed on a first surface side of a substrate. The solar cells are electrically connected to one another in series by a first conductor structure at least partially disposed on the first surface side of the substrate, forming a solar cell or supply circuit. A second conductor structure in series with the solar cell circuit is at least partially disposed on the second surface side of the substrate, forming a return harness. The supply circuit and the return harness define current paths that are opposite one another, and that are separated from one another by the substrate. The first and second conductor structures can be formed from conductive traces on the first and second sides respectively of the substrate.

Abstract: Technologies are shown for high granularity metric (HGM)-based control for smart contract execution. In accordance with some aspects, a function call associated with one or more methods of a smart contract on a blockchain is detected by identifying an entrance or exit of the function call in a kernel for smart contract execution on the blockchain. The function call is added to a function call stack, and one or more detected HGMs are identified in the function call stack. A comparison of the detected HGMs in the function call stack against one or more control rules is performed. Execution or completion of the function call is blocked based on the comparison.

Abstract: Spacecraft propulsion systems and methods featuring a first storage tank containing a metallic propellant and a second storage tank containing a non-metallic propellant are provided. A selected one of the metallic propellant and the non-metallic propellant is supplied to an electric propulsion thruster, depending on an operational mode of the spacecraft. The metallic propellant is stored at a relatively high density, while the non-metallic propellant is stored at a lower density than the metallic propellant. Moreover, the non-metallic propellant is preferably utilized to produce thrust through the electric propulsion thruster during operational maneuvers, while the metallic propellant is reserved for producing thrust through the electric propulsion thruster during end-of-life, such as deorbiting, maneuvers.

Abstract: A refuse vehicle includes a chassis, an energy storage device supported by the chassis and configured to provide electrical power to a prime mover, wherein activation of the prime mover selectively drives the refuse vehicle, a body for storing refuse therein supported by the chassis, a first hydraulic pump configured to convert electrical power into hydraulic power, a second first hydraulic pump configured to convert electrical power into hydraulic power, and a motor coupled to at least one of the body or the chassis and configured to drive the first hydraulic pump and drive the second hydraulic pump.

Abstract: A levelling laser for generating a laser projection line on a surface is disclosed. The levelling laser includes an optical projection lens with a three-dimensional lens surface. The projection lens can be described in a three-dimensional coordinates system having three axes, X, Y and Z, arranged orthogonally to one another. The Z-axis coincides with the optical axis of the projection lens. The lens surface of the projection lens has a shape with a surface inclination angle rising monotonically along the X-axis. A corresponding projection lens is also disclosed.

Abstract: Systems and methods for refueling a chemical propulsion system are provided. The systems can include multiple pressurant reservoirs to supply pressure to one or more fuel tanks. During a refueling operation, pressurant is released, fuel is added to the fuel tank, and then the fuel tank is repressurized using pressurant from a secondary pressurant tank. In other configurations, during a refueling operation pressurant is cooled to depressurize the fuel tank, fuel is added to the fuel tank, and then the pressurant is heated to repressurize the fuel tank. The systems and methods can be used to refuel operationally deployed space craft.

Abstract: Chemical propellant storage and supply systems and methods for use on spacecraft are provided. The systems and methods include a fluid pump for moving chemical propellant within the system at selected pressures. This can include operating the fluid pump to supply propellant to a thruster system at a selected pressure. A fuel tank can be refilled by connecting a propellant resupply source to the system, and operating the fluid pump to move propellant from the propellant resupply source to the fuel tank. In a system with multiple fuel tanks, the fluid pump can be operated to move propellant from a donor fuel tank to a recipient fuel tank. The chemical propellant can be stored in one or more fuel tanks at a relatively low pressure. In addition, the chemical propellant is not pressurized by a gaseous pressurant while it is stored in the fuel tank.

Abstract: The accuracy of existing machine learning models, software technologies, and computers are improved by estimating whether a particular page belongs to a same document as another page or whether the page belongs to a different document. Such document distinguishing can be based on deriving relationship information between a first feature vector representing the page and a second feature vector representing the other page. This also improves the user experience and model building experience, among other things.

Abstract: A spacecraft includes a spacecraft main body, including payload equipment disposed on an inner panel surface of at least one radiator panel, the at least one radiator panel having an exterior-facing outer panel surface. The spacecraft includes at least one electric thruster disposed proximate to an aft facing panel of the spacecraft main body. The at least one electric thruster is thermally coupled with the at least one radiator panel by way of a thermally conductive path.

Abstract: A spacecraft includes a spacecraft main body, including payload equipment disposed on an inner panel surface of at least one radiator panel, the at least one radiator panel having an exterior-facing outer panel surface. The spacecraft includes at least one electric thruster disposed proximate to an aft facing panel of the spacecraft main body. The at least one electric thruster is thermally coupled with the at least one radiator panel by way of a thermally conductive path.

Abstract: A toy figure, with an upper torso; a shoulder flange rotatably mounted on the upper torso; and an extendable arm pivotally mounted to the shoulder flange. The extendable arm may pivot with respect to both the shoulder flange and the upper torso to extend away from the upper torso, and includes an elbow that allows the extendable arm to straighten and bend. The toy figure includes an actuating mechanism disposed within the upper torso that forces the extendable arm to pivot and extend away from the upper torso. A tie rod may interconnect the shoulder flange to a portion of the extendable arm through the elbow so that so that pivotal movement of the arm around the shoulder flange causes the extendable arm to straighten.

Abstract: An enhanced video conferencing system and method includes at least two conference rooms, the conference rooms connected together electronically to permit the transmission of images and sound from one room to the other room. Each room has a large format display system for projecting images and a camera positioned with respect to the large format display system to capture images of the conference room and its participants while the participants are looking at the large format display system, without obscuring the participants' view of the display system, so as to provide the perception that the participants in one conference room are looking directly at the participants in the other conference room. The enhanced video conferencing system may also include an additional camera for capturing an image of an item located at a pre-determined location within the conference room for ultimate transmission to the other conference room for viewing.

Abstract: An enhanced video conferencing system and method includes at least two conference rooms, the conference rooms connected together electronically to permit the transmission of images and sound from one room to the other room. Each room has a large format display system for projecting images and a camera positioned with respect to the large format display system to capture images of the conference room and its participants while the participants are looking at the large format display system, without obscuring the participants' view of the display system, so as to provide the perception that the participants in one conference room are looking directly at the participants in the other conference room. The enhanced video conferencing system may also include an additional camera for capturing an image of an item located at a pre-determined location within the conference room for ultimate transmission to the other conference room for viewing.

Abstract: An improved french fried product dispensing apparatus is provided comprising a frying bath, a food hopper located above and to one side of the bath, a frying basket movable from an upright position in the frying bath to an least partially inverted position outside the bath, a device for effecting such a movement, a device for ejecting a portion of the food from the hopper into the basket when the basket is in a position between its upright position and its at least partially inverted position, the food hopper having a mechanical impeller therein to prevent bridging of food in the hopper, the hopper enclosed within a refrigerated sub-housing and providing an enclosure for insulating and refrigerating portions of food when removed from the hopper and maintained in the device for ejecting a portion of the food.