Abstract: Systems and methods for deposition-based manufacturing and quantum spin separation in space environments are disclosed herein. A method of manufacturing a film in a space environment includes melting a metal in a melting pot using concentrated solar energy and pushing the melted metal through small openings in the melting pot to produce a liquid stream. The method further includes dispersing the liquid stream into liquid drops of the melted metal and depositing the liquid drops onto a mold surface.

Abstract: Disclosed herein are analogs and derivatives of aleutianamine and methods of making the same. Also disclosed herein are methods of treating pancreatic cancer comprising administration of aleutianamine or its analogs.

Abstract: A chamber for a gas laser device includes first and second main electrodes arranged with a longitudinal direction being along a predetermined direction as being spaced apart from and facing each other in the internal space, a window arranged at a wall surface of the chamber, and a first preionization electrode arranged beside one side of the first main electrode. The first preionization electrode includes a first dielectric pipe extending along the longitudinal direction, a first preionization inner electrode arranged in the first dielectric pipe and extending along the longitudinal direction, and a first preionization outer electrode extending along the longitudinal direction, including a first end portion facing an outer circumference surface of the first dielectric pipe, and extending from the first end portion in a direction away from the first dielectric pipe. In a plane perpendicular to the longitudinal direction, a first corona discharge angle is an acute angle.

Abstract: Systems and apparatus are disclosed for mining the permafrost at the landing sites using radiant gas dynamic mining procedures. The systems can comprise a rover vehicle with an integrated large area dome for cryotrapping gases released from the surface and multi-wavelength radiant heating systems to provide adjustable heating as a function of depth. Various antenna arrays and configurations are disclosed, some of which can cooperate for a specific aiming or targeting effect.

Abstract: Omnivorous solar thermal thrusters and adjustable cooling structures are disclosed. In one aspect, a solar thermal rocket engine includes a solar thermal thruster configured to receive solar energy and one or more propellants, and heat the one or more propellants using the solar energy to generate thrust. The solar thermal thruster is further configured to use a plurality of different propellant types, either singly or in combination simultaneously. The solar thermal thruster is further configured to use the one or more propellants in both liquid and gaseous states. Related structures can include valves and variable-geometry cooling channels in thermal contact with a thruster wall.

Abstract: Systems and methods for fabrication of ceramics from celestial materials using microwave sintering and mechanical compression for space mining applications are disclosed. In one aspect, a chamber for sintering loose mineral material into solid ceramic shapes includes a plurality of zirconia insulting plates configured to clamp the mineral material and forming a cavity in which the mineral loose material is contained, and at least one dipole array configured to generate microwave energy and apply the microwave energy to the mineral material.

Abstract: Systems and methods are disclosed for mining lunar and Martian polar permafrost to extract gas propellants. The method can comprise identifying a plurality of near-polar landing sites in craters in which the surface comprises permafrost in perpetual darkness, wherein such landing sites have perpetual sunlight available at altitudes of about 100 to 200 m. A mining outpost can be established in at least one of the sites and a high altitude solar array deployed at the landing site using a lightweight mast tall enough to generate near continuous power for the outpost. Systems and apparatus are disclosed for mining the permafrost at the landing sites using radiant gas dynamic mining procedures. The systems can comprise a rover vehicle with an integrated large area dome for cryotrapping gases released from the surface and multi-wavelength radiant heating systems to provide adjustable heating as a function of depth.

Abstract: Systems and techniques for the optimized matched filter tracking of space objects are provided. In one aspect, a method of detecting faint objects includes receiving a plurality of telescope images from a telescope imaging system and performing a plurality of computational calculations on the telescope images using a plurality of search parameters to identify one or more objects moving through the telescope images. The number of the computational calculations is reduced by a priori relatively restricting a parameter space of the computational calculations.

Abstract: Systems and methods are disclosed for directing radiant energy to permanently shadowed or occasionally shadowed regions such as on the floors of craters or in valleys in lunar polar regions to provide illumination, thermal power, electricity, communications, and other services. Embodiments of the systems include reflector elements to provide diffuse illumination, focused illumination, and thermal power, structures to support the reflectors and other elements, communications devices for varied signal types, and methods for installing the system. The structure can be compactly folded and delivered to be automatically installed.

Abstract: A chamber for a gas laser device includes a first main electrode and a second main electrode arranged along a predetermined direction as being apart from and facing each other in the internal space, a window arranged at a wall surface of the chamber and transmitting light from the internal space, and a first preionization electrode arranged beside one side of the first main electrode. Here, the first preionization electrode includes a first dielectric pipe, a first preionization inner electrode arranged in the first dielectric pipe and extending along the first dielectric pipe, and a first preionization outer electrode extending along the first dielectric pipe and including a first end portion facing the first dielectric pipe with a first gap with respect to the first dielectric pipe. At least a part of the first gap is larger than 0 mm and equal to or smaller than 0.9 mm.

Abstract: A gas laser device includes a laser chamber including an opening, an electrical insulating portion blocking the opening, a first electrode, and a second electrode facing the first electrode. The first electrode includes a contact region contacting the surface of the electrical insulating portion, an opposing surface facing the second electrode, and a first curved surface included in a region between the contact region and the opposing surface and convexly curved toward an outer side of the first electrode. In a cross section of the first electrode along a surface extending in a separation direction of the first electrode and the second electrode, the contact region is located on an inner side of the first electrode with respect to the first curved surface, and the first curved surface is a part of a circumference of a circle or an ellipse which does not intersect the electrical insulating portion.

Abstract: A factory for manufacturing useful products while orbiting is space uses concentrated solar energy, high vacuum, and the low temperatures available in a space environment. Gyroscopic forces from rotating machinery are carefully controlled. Liquids, gases, and solid minerals are separated from asteroid and lunar regolith resources.

Abstract: Deployable lunar landing pads for space mining applications are disclosed. In one aspect, a landing pad for deployment on a celestial body includes a deployable surface configured to be stored in a stowed configuration on a spacecraft and be deployed into a deployed configuration on a surface of the celestial body, a landing system configured to land the landing pad on the surface of the celestial body, and a control system configured to control the landing system during landing of the landing pad on the surface of the celestial body and control the deployment of the deployable surface. The deployable surface is further configured to reduce or eliminate scattering of loose material from the surface of the celestial body in the deployed configuration.

Abstract: Omnivorous solar thermal thrusters and adjustable cooling structures are disclosed. In one aspect, a solar thermal rocket engine includes a solar thermal thruster configured to receive solar energy and one or more propellants, and heat the one or more propellants using the solar energy to generate thrust. The solar thermal thruster is further configured to use a plurality of different propellant types, either singly or in combination simultaneously. The solar thermal thruster is further configured to use the one or more propellants in both liquid and gaseous states. Related structures can include valves and variable-geometry cooling channels in thermal contact with a thruster wall.

Abstract: Systems and apparatus are disclosed for mining the permafrost at the landing sites using radiant gas dynamic mining procedures. The systems can comprise a rover vehicle with an integrated large area dome for cryotrapping gases released from the surface and multi-wavelength radiant heating systems to provide adjustable heating as a function of depth. Various antenna arrays and configurations are disclosed, some of which can cooperate for a specific aiming or targeting effect.

Abstract: Systems and techniques for the optimized matched filter tracking of space objects are provided. In one aspect, a method of detecting faint objects includes receiving a plurality of telescope images from a telescope imaging system and performing a plurality of computational calculations on the telescope images using a plurality of search parameters to identify one or more objects moving through the telescope images. The number of the computational calculations is reduced by a priori relatively restricting a parameter space of the computational calculations.

Abstract: Pneumatically supported towers for low gravity applications are disclosed herein. In one aspect, an inflatable tower for use in vacuum environments can have a membrane configured to support a load when inflated with an inflation gas to a pressures less than 100,000 pascals and greater than 0.01 pascal. The inflation gas can be chosen to have a sufficiently low boiling temperature at the inflation pressure of the membrane that the gas will not condense to a liquid or solid within a defined range of temperatures in which the tower is designed to operate. The membrane can be configured to be packaged for transport in deflated condition and rolled onto cylinders from which the membrane can be later unfurled and inflated as part of the tower inflation process.

Abstract: In a method of facilitating flight operations, a payload is coupled to a spacecraft via a payload interface. The relative alignment of the payload and the spacecraft is dynamically adjusted (e.g., for thrust alignment) while the payload remains coupled to the spacecraft.

Abstract: Systems and methods are disclosed for mining lunar and Martian polar permafrost to extract gas propellants. The method can comprise identifying a plurality of near-polar landing sites in craters in which the surface comprises permafrost in perpetual darkness, wherein such landing sites have perpetual sunlight available at altitudes of about 100 to 200 m. A mining outpost can be established in at least one of the sites and a high altitude solar array deployed at the landing site using a lightweight mast tall enough to generate near continuous power for the outpost. Systems and apparatus are disclosed for mining the permafrost at the landing sites using radiant gas dynamic mining procedures. The systems can comprise a rover vehicle with an integrated large area dome for cryotrapping gases released from the surface and multi-wavelength radiant heating systems to provide adjustable heating as a function of depth.

Abstract: A chamber device includes a housing into which a laser gas is filled, a pair of discharge electrodes generating light from the laser gas when a voltage is applied thereto, a window arranged at a wall surface of the housing and transmitting the light therethrough, a first fan causing the laser gas to flow between the discharge electrodes, a filter, a second fan rotating together with the first fan by a drive force of a drive source of the first fan, a fan-side flow path causing the laser gas filtered by the filter to flow by the second fan and a part of the laser gas to flow in a direction away from the window, and a window-side flow path communicating with the fan-side flow path and causing the laser gas flowing from the fan-side flow path by the second fan to flow toward the window.