Abstract: An androgynous fastener for autonomous robotic assembly of high performance structures is disclosed herein. The androgynous fastener is lightweight and facilitates assembly through simple actuation with large driver-positioning tolerance requirements. The androgynous fastener provides a high-strength, reversible mechanical connection and may be used in high strength-to-weight ratio structural systems, such as lattice structure systems. The androgynous fastener resists tensile and shear forces upon loading of the lattice structure system thereby ensuring that the struts of the lattice structure system govern the mechanical behavior of the system. The androgynous fastener eliminates building-block orientation requirements and allows assembly in all orthogonal build directions. The androgynous fastener may be captive in building-block structural elements thereby minimizing the logistical complexity of transporting additional fasteners.

Abstract: Software and hardware for monitoring, testing, and developing communication and electronic systems on spacecrafts. Several systems are provided to monitor, test, and control a next generation SpaceCube, including a RadHard Monitor (RHM), a Mini ASTM Board, an FMC+ ASTM Board, a Mini Evaluation Board, a MEZZ and an Automated Test Suite. The RHM are FPGA IP and hardware configured to monitor COTS components. The Mini ASTM Board connects a Mini Processor Card to an ASTM for electrical testing. FMC+ ASTM Card connects FMC and FMC+ test cards to the ASTM for electrical testing. A Mini Evaluation Board supplies all necessary power to the Mini Processor card. The MEZZ is a multi-use GSE test board that is compatible with several different development platforms in the SpaceCube to allow developers to develop and test their software. The Automated Test Suite provides functional testing of an assembled SpaceCube board.

Abstract: A brain-computer interface system includes a video processor for producing a display signal, a temporal controller for producing a plurality of repetitive visual stimulus (RVS) signals with different respective temporal aspects, a display device that receives the display signal and displays a corresponding image on a plurality of different display regions and receives the RVS signals and displays corresponding RVS in respective ones of the display regions, an electroencephalographic (EEG) sensor for sensing a visually-evoked cortical potential (VECP) signal in a user with eyes fixated on a viewed one of the display regions, and a VECP processor for processing the VECP signal to identify the respective temporal aspect of the respective RVS of the viewed display region to estimate the eye fixation location. The RVS are generated independently of the display update/refresh rate and at sufficiently high frequencies to avoid flicker perceptible to the user.

Abstract: A spacecraft computing system, including: a first processor configured to process data from a payload and a first spacecraft system; a second processor configured to process data from a second spacecraft system; an interface connected to the second processor configured to interface with a third spacecraft system, wherein the second processor is configured to monitor the first processor and to initiate the recovery of the first processor when the first processor experiences a fault, wherein the first processor's processing capacity is greater the second processor's processing capacity, and wherein the second processor is more reliable than the first processor.

Abstract: A method of manufacturing an all-solid-state battery cell includes depositing an interlayer directly onto an anode current collector; depositing a solid electrolyte onto the interlayer opposite the anode current collector; forming a cathode on the solid electrolyte opposite the interlayer, wherein the cathode contains one or more lithium-containing compounds; and applying pressure to achieve uniform contact between layers. The manufactured all-solid-state battery cell is anode-free prior to charging. The interlayer is configured such that lithium metal is deposited between the interlayer and the anode current collector during charging, the interlayer prevents contact between the lithium metal and the solid electrolyte, and the interlayer has a greater density than a density of the solid electrolyte.

Abstract: A dynamic function allocation (DFA) framework balances the workload or achieves other mitigating optimizations for a human operator of a vehicle by dynamically distributing operational functional tasks between the operator and the vehicle's or robot's automation in real-time. DFA operations include those for aviation, navigation, and communication, or to meet other operational needs. The DFA framework provides an intuitive command/response interface to vehicle (e.g., aircraft), vehicle simulator, or robotic operations by implementing a Dynamic Function Allocation Control Collaboration Protocol (DFACCto). DFACCto simulates or implements autonomous control of robot's or vehicle's functional tasks and reallocates some or all tasks between a human pilot and an autonomous system when such reallocation is preferred, and implements the reallocation.

Abstract: A method for testing a battery cell includes directing a laser radiation from a laser at a radiation-receiving location on a can of the battery cell to trigger a thermal runaway event. A power, a wavelength, and a beam size of the laser radiation are selected based on a test stability of the battery cell when triggering the thermal runaway event. The test stability includes a likelihood that the can will breach in response to triggering the thermal runaway event. The method also includes ceasing to contact the radiation-receiving location with the laser radiation in response to the thermal runaway event.

Abstract: An anti-phase rotor system for an aircraft may include at least one rotor with at least two rotor blades. The aerodynamic profile of these two blades may be selected to create counteracting blade vortices to break up harmonic reinforcement due to the rotor blade passage. The aerodynamic profile may create a non-planar motion of one or more rotor blade passages, whereby the individual rotor blades are not co-planar during the rotation of said rotor. The rotor system may include a duct, which may include stationary vanes or struts configured in a manner so as to break up harmonic excitation to the rotor. The interior area of the duct at the area of the blade rotation may be designed in a manner so as to create a destructive rotor blade tip vortex interference.

Abstract: Additive manufacturing systems and methods are disclosed. A housing includes a passageway having first and second open ends. A material is fed through the passageway and exits its second open end. A friction stir weld (FSW) bobbin pin tool is mounted in the housing with a radial edge of the pin tool's annular volume disposed adjacent to the second open end of the passageway. The annular volume is adapted to receive a substrate. The FSW bobbin pin tool is operable to be rotated so that the substrate and the material exiting the second open end of the passageway are plasticized in the annular volume for deposition onto the substrate.

Abstract: Methods and systems for the laser surface treatment on stainless steel alloys and nickel alloys may include a computer may be programmed to set a laser path corresponding to a predetermined geometric pattern. A laser may be coupled to the computer and apply a pulsed laser beam to a contact surface of the substrate along the predefined geometric pattern. The pulsed laser beam may have a laser power between 0.1 W and 100 W, single pulse fluence 1 mJ/mm2 and 1025 mJ/mm2 and a laser speed between 25.4 cm/s and 127 cm/s. The laser may generate an open pore oxide layer on the contact surface of the substrate with a thickness of 0.1-1 ?m, an open pore distance of 0.05-1 ?m. The open pore oxide layer may have a topography corresponding to the predefined geometric pattern. The topography may contain open pore structures and promote adhesive bond performance.

Abstract: Various embodiments relate to a light detecting and ranging (LiDAR) system including: a space-qualified transmitter including a space-qualified microelectromechanical system (MEMS); a space-qualified receiver; a space-qualified short-range imager connected to the space-qualified receiver; a space-qualified long-range imager connected to the space-qualified receiver.

Abstract: A space based multi-band GPS/GNSS navigation system, including: RF card to receive and process the two different received navigation signals; a space grade navigation processor configured to: execute processor instructions to process the two different received navigation signals to produce position, velocity, and time information; and process measurements using a Kalman filter for enhanced performance at high altitude.

Abstract: A visual inspection posable invertebrate robot (VIPIR) borescope camera system can inspect components in difficult to reach locations. The system enables dexterous robotic inspection of worksites and areas that were heretofore impossible to inspect via extravehicular activities (EVA) and fixed situational awareness cameras. VIPIR may include: (1) a main drive assembly; (2) a reel system; (3) a video borescope assembly (VBA); (4) an enhanced motorized zoom lens (EMZL); (5) a fixed camera assembly (FCA); (6) a support structure; and/or (7) a main electronics box (MEB).

Abstract: A radio-frequency identification (RFID) antenna assembly, per an implementation, includes a number of multiplexer modules coupled with one another. Radio frequency (RF) signals are received from an RFID reader. One or more of the multiplexer modules has a switch with multiple output ports. An antenna connects with one of the output ports and, per an implementation, an encoder connects with another of the output ports. The multiplexer module(s) may also have a first rectifier for rapid self-powering capabilities, and a second rectifier for more robust self-powering capabilities.

Abstract: Various examples are provided related to measuring surface tension. In one example, a method includes levitating a sample using electrostatic levitation; applying a signal to at least one electrode to excite the sample into a n=3 mode of oscillation; capturing images of the sample with a respective image being associated with a particular frequency that is applied to the sample when the respective image is captured; quantifying sample resonance using a projection method of Legendre polynomials based on the plurality of images; and determining a measured resonance frequency of the sample by an analysis of the sample resonance. The sample can be levitated using a feedback-controlled voltage and the applied signal can be swept over a range of frequencies. A system including electrodes, a position sensor, a camera device, and at least one computing device can be used to carry out the method.

Abstract: A method of coating a substrate with a white molecular coating. A colloidal based primer is prepared having on a mass basis between 30-40% suspensions of fine-sized spherical particles of nonporous silica dispersed in liquid phase. The primer is applied to the substrate and allowed to dry. A molecular adsorber coating is prepared by treating a zeolite with a colloidal silica binder thereby providing a treated pigment having a mass ratio of the colloidal silica to the zeolite is in a range of 2.0 to 2.6, then processing the treated pigment into a powder thereby facilitating sprayability and then mixing said treated zeolite with a colloidal solution containing silica. The coating is then sprayed onto the primer and allowed to dry. The resultant coating provides adequate bond stability and strength necessary for flight applications within an environment for vacuum of space applications.

Abstract: A magnetohydrodynamic (MHD) flow control mechanism is described which substantially improves the existing processes in that smaller magnetic fields, requiring far less mass, are placed away from the forebody of the spacecraft to produce Lorentz forces that augment the lift and the drag forces for guidance, navigation, and control of the spacecraft.

Abstract: The present disclosure is directed to a system including a nuclear thermal rocket or a nuclear reactor, at least one nuclear electric thruster coupled to the nuclear thermal rocket or the nuclear reactor, and a Nuclear Thermionic Avalanche Cell (NTAC) configured to generate electrical power. The NTAC cell may be positioned around a nuclear reactor core of the nuclear thermal rocket or the nuclear reactor, and the nuclear electric thruster may be powered by the NTAC generated electrical power.

Abstract: The present invention relates to a single-board solid state data recorder (SSDR) card configured for use in a 1U CubeSat payload form-factor multi-purpose architecture, which includes: a field programmable gate array (FPGA): a plurality of NAND storage banks of non-volatile NAND Flash storage, the plurality of NAND storage banks which store operational data, each of which is controlled by a NAND Flash controller which controls the signaling of the plurality of NAND storage banks and reading and writing to the plurality of NAND storage banks; and a plurality of SpaceWire nodes and a plurality of multi-gigabit transceivers which command the SSDR card and read/write data to the SSDR card; wherein the plurality of NAND Flash memory banks is independently controlled and independently powered.

Abstract: Methods for making layered materials and layered materials including high atomic number metals and metal alloys adhered to surfaces are provided. Such surfaces may be oxygen or hydroxyl rich surfaces. Certain methods include depositing a tie down layer of a first metal or metal alloy particles onto a first surface of base material and depositing a high atomic number metal or metal alloy layer onto the first surface after depositing the tie down layer, wherein particles comprising the high atomic number metal or metal alloy layer have a higher atomic number than the first metal or metal alloy particles.