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WO/2021/107051A1 |
For the purpose of allowing a plurality of management business operators managing space objects flying in space to efficiently share and conduct a hazard analysis, a plurality of space traffic management apparatuses (100) are connected t...
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WO/2021/102669A1 |
An autonomous maintenance method for ultra-low orbit satellites. The method comprises: step 1: setting a working orbit range of a satellite, and estimating the magnitude of atmospheric drag; step 2: analyzing the magnitude of noise of an...
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WO/2021/105146A1 |
The invention relates to a coupling means (10, 18, 19), especially an androgynous coupling means (10, 16, 17), exhibiting male and/ or female coupling sections (11, 12), wherein the coupling means is configured for form fit coupling with...
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WO/2021/107056A1 |
For the purpose of performing flight safety measures by satellite group, a space information recorder (101) is mounted on: a mega-constellation satellite business device, which is a business device that manages a constellation of 100 or ...
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WO/2021/096006A1 |
According to an embodiment of the present invention, a system for concurrently transmitting wireless power and data between an artificial satellite and a satellite payload by using a relay resonator comprises: a connection part which con...
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WO/2021/094719A1 |
A device (100) for generating a force is provided. The device comprises at least one multi-layer structure (110). The multi-layer structure comprises an anode layer (112), a cathode layer (114); and an active layer (116) between the anod...
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WO/2021/093549A1 |
A damping vibration attenuation structure for a space satellite-borne instrument, the structure comprising a supporting cylinder main body (1), damping assemblies (2) and a vibration attenuated assembly (3). The supporting cylinder main ...
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WO/2021/096000A1 |
The present specification relates to a safe landing point search device for searching for a safe landing point for an unmanned exploration device which lands and explores a celestial body, the safe landing point search device comprising:...
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WO/2021/091424A1 |
The invention relates to rocket and space technology and is intended for the landing of vertical landing rockets and detached reusable stages. The present system for receiving vertical landing rockets comprises a landing platform, wherei...
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WO/2021/090361A1 |
[Problem] To provide a spacecraft having a more effective arrangement of amplifiers. [Solution] Provided is a spacecraft comprising: a main body having a housing space for housing an electronic device within; an oscillator configured to ...
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WO/2021/088818A1 |
Disclosed is an auxiliary hydraulic supporting device for a rocket (6), the device comprising a hydraulic system (1), a guide supporting cylinder (2), an elastic supporting assembly (3) and a rocket bracket (4), wherein the hydraulic sys...
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WO/2021/089167A1 |
The invention relates to a separation system that dispenses a satellite from a launch vehicle along a dispensing axis, with a first ring for mounting to the launch vehicle and a second ring for mounting to the satellite and a deployment ...
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WO/2021/089938A1 |
The invention relates to a method for tracking, by means of a space vehicle (101), a target on an orbital trajectory, the method comprising an acquisition phase (504, 505) which comprises the steps of: - activating a lidar; - acquiring s...
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WO/2021/083858A1 |
The invention relates to a drive assembly for a satellite (1), comprising: - an electron emitting device (5), which is designed to emit electrons; - a tether (3) comprising: - a carrier element (31); - an energy recovery structure (32), ...
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WO/2021/087076A1 |
In an aspect, an artificial selenomelanin material comprises: one or more selenomelanin polymers; wherein the one or more selenomelanin polymers comprise a plurality of covalently bonded selenomelanin base units; and wherein a chemical f...
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WO/2021/081687A1 |
A method for use in monitoring a satellite standalone unit failure based on a single indicator threshold, comprising the following steps: providing a standalone unit indicator analytic function (302); providing a failed service handling ...
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WO/2021/085217A1 |
The present invention realizes efficient orbital transfer without complicating structure. A tether storage unit 5 for artificial satellites includes: a housing 11; a tether 13 which is stored in the housing 11 so as to be extendable outw...
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WO/2021/081389A1 |
A system for delivery to space on a launch vehicle includes a first payload configured to directly couple to an adapter structure of the launch vehicle, a second payload configured to directly couple to the adapter structure of the launc...
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WO/2021/081427A1 |
Provided herein are various leptonic power sources, leptonic control systems, and leptonic-powered engines. In one example, an apparatus includes a housing having apertures through which material can enter and exit, and an anode coupled ...
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WO/2021/074910A1 |
An on-orbit servicing spacecraft (1) comprising an engagement system (4) to engage a space vehicle or object (5) to be serviced or tugged, so as to form a space system (6); and an electronic reaction control system (7) to cause the space...
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WO/2021/072464A1 |
The invention relates to a parachute system (1) for a projectile, preferably an unmanned projectile, wherein the parachute system (1) comprises a parachute (2) and a gas-operated trigger system (3) for the parachute (2), which is designe...
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WO/2021/068554A1 |
Disclosed is a spacecraft nutation inhibition method for low-orbit geomagnetic energy storage in-orbit delivery. The method comprises: S1, enabling a delivery connection rod (7) to be slidably connected to two mass blocks (72) in a lengt...
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WO/2021/071567A1 |
Embodiments of the present disclosure generally relate to protective coatings on an aerospace component and methods for depositing the protective coatings. The protective coating can be anti-coking coatings to reduce or suppress coke for...
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WO/2021/065734A1 |
The purpose of the present invention is to provide a notification of an appropriate intrusion warning by determining whether debris intrudes into the orbit region of a satellite constellation. A passage determination unit (110) determine...
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WO/2021/064350A1 |
A : spacecraft attitude control system comprising • at least one attitude control device (2), the attitude control device comprising • first and second magnets (3, 4) having magnetic dipole moments Ml and M2 respectively, each magnet...
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WO/2021/063775A1 |
The invention relates to a device (500) for a satellite laser distance measurement, comprising a base segment (520) and an optical segment (522) which is supported by the base segment (520) and has a telescope mounting (510) with an azim...
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WO/2021/060490A1 |
The purpose herein is to more accurately assist the avoidance of collisions of space objects such as satellites and space debris in outer space. A recorder processing unit (110) acquires, from a management business device (40) used by a ...
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WO/2021/060491A1 |
To appropriately manage the disclosure of information on the orbit of a satellite constellation, an information management device (1000) is installed in at least one of a plurality of management business devices, each of which manages a ...
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WO/2021/059424A1 |
A satellite visibility assignment device (1) comprises a visibility unit setting section (21), a visibility unit selection section (22), and an optimal calculation unit (23). The visibility unit setting section (21) sets a visibility uni...
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WO/2021/061079A1 |
The present invention relates to a vibration isolator (10), which is arranged identically and adjacently in multiple numbers on the adapter (3), comprises an upper connector (20) adjusted to be connected to a payload (2) placed on an ada...
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WO/2021/059134A1 |
A spacecraft servicing system to provide in-orbit servicing through the umbilical connectors of a spacecraft. In one embodiment, a manipulator arm maneuvers a servicer umbilical to form an electrical connection between a servicer spacecr...
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WO/2021/060492A1 |
The purpose of the present invention is to assist a suitable avoidance action, when a collision of space objects in outer space is predicted in advance, and a storage unit (140) stores orbit prediction information (51) which is a predict...
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WO/2021/052087A1 |
A manipulation method suitable for a non-redundant SGCMG group. The method comprises the steps: 1) determining, according to configurations and synthetic angular momentums of n SGCMGs, nominal frame angle vectors of the configurations of...
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WO/2021/051072A2 |
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WO/2021/048589A2 |
It is a fact that the degree of traction and friction is correlated to the self-weight of the tyre and the exerted load. In addition, the more the exerted or supported load, the more difficult it is to roll the tyre on that surface. Ther...
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WO/2021/044142A1 |
There is provided a thermal management apparatus for use with a vehicle comprising: a chassis in thermal contact with one or more first components that require thermal management and one or more second components that require thermal man...
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WO/2021/046209A1 |
Disclosed herein is a spacesuit including a liquid cooling ventilation garment, a soft exoskeleton, at least one biometric sensor, and an electronic controller in electronic communication with the liquid cooling ventilation garment, the ...
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WO/2021/046044A1 |
The invention provides an electrothermal RF plasma production system and thruster design, and associated components, that may use water vapor or other condensable propellants. The plasma production system and thruster design may be used ...
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WO/2021/037785A1 |
The present disclosure relates to deployable structures, to methods and apparatus for deployment of deployable structures, and to associated manufacturing methods. Such deployable structures suitably comprise components for space structu...
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WO/2021/035757A1 |
Provided is a moon-based environment simulation device (100), comprising a moon ground simulation system (101) and a moon rock simulation system (103) which are arranged in a connection manner, the moon ground simulation system (101) is ...
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WO/2021/037787A1 |
The present disclosure relates to deployable structures, to methods and apparatus for deployment of deployable structures, and to associated manufacturing methods. Such deployable structures suitably comprise components for space structu...
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WO/2021/039652A1 |
A debris removal satellite (300) comprising a capture device (135), a chemically-propelled thruster (341), and a propellant tank (342) that stores chemical fuel. A solar cell paddle (371) can be operated in an orbit having a higher orbit...
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WO/2021/042076A1 |
Systems and methods described herein include collapsible and deployable antenna structures including shape memory composite components.
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WO/2021/037786A1 |
The present disclosure relates to deployable structures, to methods and apparatus for deployment of deployable structures, and to associated manufacturing methods. Such deployable structures suitably comprise components for space structu...
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WO/2021/031686A1 |
A transfer type contra-rotating geomagnetic energy storage-release delivery system and method therefor, the system comprising a control system, a three-axis control moment canceller and an energy system which are arranged on a delivery m...
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WO/2021/031740A1 |
The invention provides a multi-purpose planet rover, relating to the technical field of planet explorations. The multi-purpose planet rover comprises: a container body, wherein first rotating wheels are respectively mounted on left and r...
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WO/2021/026412A1 |
A modular and scalable system to transfer space articles between space orbits. In one embodiment, the system employs a rendezvous vehicle which docks with a space article in an initial orbit, the connected stack then docking with a locom...
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WO/2021/022253A1 |
Systems and methods for controlling satellites are provided. In one example embodiment, a computing system can obtain a request for image data. The request can be associated with a priority for acquiring the image data. The computing sys...
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WO/2021/019827A1 |
Provided is a system for satellite operators by which information relating to retrieved ground stations can be easily obtained. An information processing device according to the present technology is provided with a user interface unit w...
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WO/2021/014137A1 |
A device comprising a first member (12) for supporting a user (200); and a second member (14), attached to the first member (12), comprising a counterbalance portion (16). The first member (12) and the second member (14) are each moveabl...
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