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WO/2023/007579A1 |
[Problem] The present invention addresses the problem of providing a novel propulsive-force generating device, which employs a centrifugal force, and which resolves the drawbacks of conventional propulsive-force generating devices that e...
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WO/2023/009818A1 |
A system for harvesting solar energy on a spacecraft includes a stiff substrate layer (205) and a working layer (208) disposed on the substrate layer (205) to provide at least one of a photovoltaic or a reflective function. In a first op...
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WO/2023/007886A1 |
[Problem] This invention addresses the problem of providing a safe and comfortable propulsive-force generation device that uses centrifugal force, which does not affect the lower world, instead of a propeller, a screw, or the like, which...
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WO/2023/008245A1 |
According to the present invention, when a de-orbiting satellite, which is one among artificial satellites belonging to a first satellite constellation (101), de-orbits from an orbit of a first orbital altitude band and descends, a secon...
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WO/2023/008145A1 |
A cloud computing system (1) comprises: geostationary satellites (10) each equipped with a computer (11) and a cloud data center (12); a low Earth orbit satellite constellation (20) including a plurality of communication satellites (30);...
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WO/2023/001414A1 |
It is disclosed a method of manufacturing a spacecraft comprising selecting an outer cover material for the spacecraft, the outer cover material having an inner surface and an outer surface, said outer surface being electrically conducti...
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WO/2023/004205A1 |
This invention relates to devices and methods that convert primary energy of a vehicle to a secondary energy. Previously, the novelty of utilizing the kinetic energy of celestial bodies as a resource for work on power plants was unfounde...
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WO/2023/285761A1 |
The invention relates to a separation device (1) comprising a release ring (5) able to slide along a segmented nut (7), the release ring (5) being configured to move between a first position, in which the segments of the nut (7) are main...
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WO/2023/286281A1 |
An observation planning device (1) comprises: an observation request acquisition unit (11) that acquires observation request information requesting observation of an area to be observed; an observation opportunity identification unit (12...
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WO/2023/287922A1 |
Material transfer interfaces for space vehicles, and associated systems and methods are disclosed. A representative system includes a first coupler configured to be carried by a first space vehicle, and a first valve device carried by th...
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WO/2023/286435A1 |
[Problem] To lessen the burden on users by enabling flexible control of communication lines according to service requirements when realizing satellite formation flight. [Solution] In order to control a movement body group involved in for...
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WO/2023/288335A2 |
A ground station communicates with a satellite having a field of view (FOV), the satellite directly communicating with user equipment (UE) over uplink signals and downlink signals. The ground station has a Dynamic Time Division Duplex (D...
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WO/2023/286861A1 |
An ionized body collecting device (1) according to the present invention is characterized by being provided with: one or a plurality of container main bodies (2) having a peripheral wall (2A) and a bottom wall (2B), and having an opening...
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WO/2023/285432A1 |
A satellite (140) for operation in orbit around the earth comprises an ADCS (131, figure 1) configured for mechanically steering the satellite in the azimuth direction to prolong a dwell time (1105), during which a selected target is vis...
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WO/2023/281282A1 |
A docking structure (1, see figure 1) for a satellite includes a magnetic plate (2) and a housing (10, 12) for mounting and constraining the magnetic plate (2). The magnetic plate includes an outer face and an inner face. The magnetic pl...
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WO/2023/281632A1 |
A capturing device (14) includes a driving mechanism control unit that drives one or more driving mechanisms (21a, 21b) to feed a tape-like enclosing member (31) toward the outside of a housing (32) by a target feed amount. When a space ...
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WO/2023/282949A2 |
Methods, devices, and systems are described for a core of a space habitat. The core includes a plurality of internal beams extending a length of the core. The core also includes a plurality of end rings at a first end of the core and a s...
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WO/2023/282948A2 |
Methods, devices, and systems are described for a bracket fixture for securing a load to a soft goods layer in a space habitat. The bracket fixture includes a base having a plurality of sides, the plurality of sides having a pin parallel...
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WO/2023/276031A1 |
[Problem] To provide a new technology for utilizing formation flight of a plurality of artificial satellites having light sources in the entertainment field. [Solution] The present invention is an artificial satellite control device whic...
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WO/2023/276030A1 |
[Problem] To provide a novel technology that uses flight by a plurality of satellites that each have a light source for entertainment. [Solution] The present invention is an artificial satellite control device that controls the plurality...
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WO/2023/278005A1 |
Methods, devices, and systems are described for a mounting flange and bracket for a space habitat. The bracket system couples a bladder of a space habitat to a cylindrical core. The bracket system includes a soft goods layer configured t...
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WO/2023/276029A1 |
[Problem] To provide a new technology for utilizing formation flight of a plurality of artificial satellites having light sources in the entertainment field. [Solution] The present invention provides a content provision device which prov...
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WO/2023/275970A1 |
[Problem] To provide a novel and improved information processing device, an information processing method, and a program, which are capable of improving robustness of a camera with regard to rotation, when identifying stars corresponding...
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WO/2023/278001A1 |
A navigation processing system includes at least one processor configured to execute operational instructions that cause the at least one processor to perform operations that include generating navigation data. A data stream is generated...
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WO/2023/276033A1 |
[Problem] To provide a novel technology which utilizes, in the entertainment field, flight control by a plurality of artificial satellites having a light source. [Solution] The present invention is an artificial satellite control system ...
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WO/2023/276032A1 |
[Problem] To provide a novel technology that utilizes formation flights by a plurality of satellites with light sources in the entertainment field. [Solution] The present invention is a satellite control device that controls a plurality ...
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WO/2023/276028A1 |
[Problem] To provide a novel entertainment application for flight control of a plurality of artificial satellites that have a light source. [Solution] The present invention is an artificial satellite control device that controls a plural...
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WO/2022/271789A1 |
In an embodiment, there is provided a method for determining a spacecraft instantaneous velocity using starlight. The method includes determining, by a star pairing module, a plurality of star pairs in a selected star field image. The se...
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WO/2022/270337A1 |
A backup satellite group (22) including a plurality of satellites (30) stands by at an orbital altitude lower than the orbital altitude of a stationary operation satellite group (21) in a satellite constellation (20). When a satellite (3...
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WO/2022/269597A1 |
A connection system is provided for releasably connecting a first component and a second component in a first direction parallel to a reference longitudinal axis, including one or more locking devices and an actuator. Each locking device...
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WO/2022/264177A1 |
Electromagnetic propulsion system for spacecraft movement without the emission of reaction mass, characterised in that it comprises two arms (10) which share one of their vertices at a point called feedpoint (14); said feedpoint (14) bei...
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WO/2022/261423A1 |
A pair of interconnected vertical solar arrays at two preselected lunar sites are provided. A cable transmits power between one of the vertical solar arrays and the other vertical solar array, so that one of the vertical solar arrays can...
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WO/2022/258123A1 |
This is a propulsion motor with a closed system and without reaction The way it works is to produce impulse in a plurality of coordinated physical steps. Step 1: The conversion of low voltage electrical energy LVCD into high current HVDC...
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WO/2022/259966A1 |
Provided is a satellite monitoring device having a reception processing unit that receives a plurality of first data groups outputted from a plurality of satellites and expressed in a corresponding format unique to each of the plurality ...
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WO/2022/254398A1 |
Device for disinfecting at least one working volume (5) in an artificial space environment (2), comprising a concentrator (6) of solar radiation associated with the at least one working volume (5), and filtering means (7) for selecting a...
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WO/2022/255405A1 |
A liquid tank (oxidant tank 2) comprises: a cylindrical seamless tank body 21 with both end portions having a decreasing diameter toward ends; and a plurality of annular baffles 221 disposed in the tank body 21, and spaced apart from eac...
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WO/2022/254327A1 |
A data acquisition system for a satellite (10) comprises at least one camera (2), a device for controlling ambient parameters and processing radiofrequency signals (3) and a microprocessor (4). The camera (2) can be activated so as to ac...
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WO/2022/253837A1 |
The invention relates to a profile section (34) for an equipment (26) support panel (27). Said profile section is formed in one piece, comprising a tube (38) suitable for forming a heat pipe by introducing and confining a heat-transfer f...
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WO/2022/249833A1 |
An integrated data library (300) is referenced by: a monitoring satellite group (110G) for tracking a flying object (10); a ground-based monitoring facility (120) for controlling the monitoring satellite group (110G); a communication sat...
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WO/2022/248418A1 |
A thermal power reactor (100) is provided. The thermal power reactor (100) includes a reactor core (102; 202; 410; 502) arranged to generate thermal energy and a solid state thermal conductor (106; 206; 406) including a graphene based me...
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WO/2022/249832A1 |
A communication satellite (200A) flies in an orbit (21) of orbital inclination angle θideg and is equipped with a communication device (51) having a view change range of ±θideg with respect to a +X axis about a Z axis, with the direct...
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WO/2022/249428A1 |
A satellite deceleration device having a ranging function according to the technology of this disclosure comprising: a pulsed light source (39); a second light output part (27) which outputs, to a space, light output from the pulsed ligh...
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WO/2022/249430A1 |
A device for changing the trajectory of an object in space according to the disclosed technology includes: light sources (2a, 2b, ...) that output light signals on two or more wavelengths; a filter controller (16) that determines a trans...
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WO/2022/249429A1 |
A device for measuring the distance to an object in space according to the disclosed technology includes: light sources (2a, 2b, ...) that output light signals on two or more wavelengths; a filter controller (16) that determines a transm...
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WO/2022/243543A1 |
A thermal management system (5) for a magnetoplasmadynamic thruster (10) for a space craft is disclosed. The thermal management system (5) is located between at least one superconducting magnet (120) and a plasma discharge unit (15 and c...
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WO/2022/245772A1 |
An apparatus comprises both a first side and a second side that is opposite the first side. The apparatus includes a plurality of photovoltaic cells disposed on the first side of the substrate and a plurality of microwave antennas dispos...
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WO/2022/237965A1 |
A vehicle for supersonic or hypersonic flight comprises a thermal rocket engine (lb) with a nozzle (2) and an active cooling system (8). The active cooling system cools a heat shield (6, 7). A working fluid absorbs heat inside the active...
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WO/2022/238660A1 |
The invention relates to a spacecraft (1) for the distribution of electrical energy to client craft (2) at points situated in free space, in orbit and/or on a celestial body, the spacecraft (1) comprising a main structure (10) equipped w...
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WO/2022/234669A1 |
A thrust generating device according to the present invention is for generating thrust in an object by irradiating the object with a laser, the thrust generating device comprising: a laser generating device that generates first laser lig...
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WO/2022/229546A1 |
The invention relates to a reflective satellite (1) comprising at least one curved reflection surface (11), the satellite (1) being characterised in that it comprises at least one load-bearing structure (10) connected to at least four po...
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