| Document |
Document Title |
|
WO/2023/025846A1 |
The present invention relates to a power conversion system for electrically-powered thrusters located on and/or inside a satellite.
|
|
WO/2023/024968A1 |
A variable-stroke self-adaptive adjustment quasi-zero stiffness device and a parameter checking method, comprising: an integrating sphere, a target, a collimator, a pointing measuring instrument, disturbance sources, an inertia simulatio...
|
|
WO/2023/027679A1 |
Proposed is a stationary ion/plasma engine comprising: a discharge chamber having an annular ionization and acceleration channel and a bottom with an inner seating surface for an anode, said chamber being made of an electrically insulati...
|
|
WO/2023/025942A1 |
A reconfigurable, modular, and scalable space infrastructure which provides a large diversity of services on demand in space, comprising a master truss (101) for housing systems of the space infrastructure to provide several services thr...
|
|
WO/2023/026011A1 |
The invention relates to a spacecraft comprising: a frame (4), an electrical device (1) supplied and/or controlled by electric cables, and an orientation system for orienting the electrical device (1), the orientation system comprising: ...
|
|
WO/2023/027893A1 |
Technology is disclosed for a spacecraft launch restraint and dispensing structure. Stacks of spacecrafts (102) may be arranged around a central post (104). The dispensing structure has primary tie-down mechanisms (120) that axially clam...
|
|
WO/2023/024203A1 |
The present invention relates to the technical field of spacecraft control, and relates to a sun-oriented directional solar wing driving device. According to the sun-oriented directional solar wing driving device, two gear rings are resp...
|
|
WO/2023/026063A1 |
Spacecraft Heat Shield A deployable spacecraft atmospheric-entry heat shield (30, 40, 50, 60) is configured in a flasher pattern with a transformable polyhedral-surface. The transformable polyhedral-surface has a plurality of sectors (2,...
|
|
WO/2023/024049A1 |
The invention relates to the technical field of ventilation apparatuses, in particular to an efficient aerospace ventilation device with a heating function. In order to solve the problem of poor air quality due to most of the existing ve...
|
|
WO/2023/024311A1 |
Disclosed is a flexible space capsule, comprising a pneumatic apparatus, a solar power generation apparatus and a rotating apparatus. A capsule body comprises a first capsule body, a second capsule body and a third capsule body. Capsule ...
|
|
WO/2023/021188A1 |
A detector module (100, 300, 400, 500, 600, 802, 1102, 1604, 1610, 1614) for image capture, in particular for an optoelectronic image capture system (200, 700, 800, 900, 1000, 1100) for an aircraft, such as a spacecraft, comprising a mai...
|
|
WO/2023/012559A1 |
An aerial vehicle engine is proposed which may be powered an adjustable, vortex-based virtual aerospike engine. The vehicle may also include a combustion chamber which may be coupled to the exit nozzle. The combustion chamber may include...
|
|
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...
|
|
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...
|
|
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...
|
|
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...
|
|
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);...
|
|
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...
|
|
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...
|
|
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...
|
|
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...
|
|
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...
|
|
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...
|
|
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...
|
|
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...
|
|
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...
|
|
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...
|
|
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 ...
|
|
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...
|
|
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...
|
|
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...
|
|
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...
|
|
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...
|
|
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...
|
|
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...
|
|
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...
|
|
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 ...
|
|
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 ...
|
|
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...
|
|
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...
|
|
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...
|
|
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...
|
|
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...
|
|
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...
|
|
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...
|
|
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 ...
|
|
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...
|
|
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...
|
|
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...
|
|
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...
|
