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WO/2021/150566A1 |
A high data rate distribution network for low-earth orbit (LEO) satellite constellations includes multiple LEO constellations, each constellation including a number of LEO spacecraft orbiting in a LEO plane that are all connected togethe...
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WO/2021/149553A1 |
The present invention pertains to an electroconductive flexible conductor provided with: a belt-like flexible resin substrate; and an etched metal foil layer which longitudinally extends from one end of said substrate to the other end th...
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WO/2021/151035A1 |
An orbital delivery system includes a exo-atmospheric system arranged along an orbital or sub-orbital trajectory. The exo-atmospheric system includes a propulsion system to adjust an orientation responsive to a signal to begin a reentry ...
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WO/2021/149485A1 |
The present technology relates to a display control device, a display control method, and a program that make it possible to verify images in real time. A display control device that comprises a reception unit that receives low-capacity ...
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WO/2021/144571A1 |
The present invention relates to an assembly apparatus for assembling components of spacecraft in space. The assembly apparatus comprises: a core platform (7); and a mobile platform (4) comprising an end effector configured to perform an...
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WO/2021/146231A1 |
Thermal barrier coatings for substrates comprising titanium. The thermal barrier coating may include a bond layer, an insulating layer, and a sealant layer. The bond layer may include titanium, a titanium alloy, an intermetallic compound...
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WO/2021/143428A1 |
An electromagnetic locking and releasing mechanism for satellite-rocket separation, and an electromagnetic locking and releasing method. The electromagnetic locking and releasing mechanism comprises: a frame (1), an ejection unit, a sate...
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WO/2020/254984A9 |
An aerodynamic louver system used in one or more of the following operations: control, adjust, or stabilize, aid in controlling, adjusting or stabilizing a spacecraft's orientation, angle of attack, lift, or position. There could be mult...
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WO/2021/141198A1 |
The present invention relates to a solar panel to which a high-damping stacked reinforcement part is applied and, more specifically, to a solar panel to which a high-damping stacked reinforcement part is applied, comprising: a power gene...
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WO/2021/135023A1 |
Disclosed is a method for tailoring for satellite random vibration and noise tests on the basis of area-to-mass ratio, and the method is used to tailor a random vibration test and a noise test in a satellite ground verification test. The...
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WO/2021/136851A1 |
Hold-down and release device (1), suitable for hold-down and release of at least two releasable bodies (4, 3) with respect to a support structure (2), that comprises: - a proximal subassembly (5) suitable for being attached to the suppor...
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WO/2021/137302A1 |
A method and system for activating thrusters of a vehicle for trajectory-tracking control of the vehicle. A transfer orbit generator to generate a transfer orbit for the vehicle from an initial orbit to a target orbit, and a feedback sta...
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WO/2021/130457A1 |
The invention relates to a support structure (41) for a spacecraft, comprising a first side wall (30), a second side wall (32) which is parallel to and opposite the first side wall, a third side wall (22) attached at least to the first s...
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WO/2021/131719A1 |
A spacecraft according to the present disclosure comprises: an orientation control actuator that controls the orientation of the spacecraft; an imaging device that receives optical communication signals from other spacecrafts; and an ori...
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WO/2021/128448A1 |
A propulsion method based on liquid carbon dioxide phase transition and a propulsion apparatus, wherein carbon dioxide in a liquid phase state is contained within a thermally insulated container (1), an instant heating module (2) perform...
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WO/2021/126010A1 |
The invention relates to the field of space technology, and more particularly to systems for docking and undocking spacecraft or parts thereof. A docking and mounting module consists of a docking device and an active mounting mechanism. ...
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WO/2021/119768A1 |
(57) This invention relates to a power supply module for nanosatellite systems which will find application in the field of space technology and satellite communications, and in particular for powering nanosatellites. The created power su...
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WO/2021/126821A1 |
Various systems and methods of a layered tile insulation system of a space vehicle, configured to withstand vibration, high temperatures, and extreme thermal gradients, are disclosed. The layered tile insulation system can include at lea...
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WO/2021/122958A1 |
The invention relates to a position control device (1) for a satellite, comprising at least one high-power torque wheel (2) for applying a torque to the satellite during a position control manoeuvre and at least one supercapacitor (3), t...
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WO/2021/119851A1 |
The present disclosure relates to a robotically controlled satellite refueling tool and associated robotically controlled support and site preparation tools which facilitates on-orbit refueling by teleoperation of fill/drain valves of va...
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WO/2021/122184A1 |
The invention relates to a method for assembling devices on a satellite structure, comprising successive steps of: - attaching (61) the devices to a first face of a plate drilled with a through-hole provided with a fluid connector; - on ...
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WO/2021/126009A1 |
The invention relates to the field of space technology, and more particularly to systems for docking and undocking spacecraft or parts thereof. The present spacecraft docking device for a two-step docking process consists of an extendabl...
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WO/2021/123661A1 |
The invention relates to a device for processing (30) orbital data which is configured to be in communication with space listening sensors (24, 26, 28), the processing device (30) comprising a computing unit configured to determine the o...
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WO/2021/123663A1 |
The invention relates to a device (30) for processing orbital data, which is configured to be in communication with space listening sensors (24, 26, 28); the processing device (30) comprising a computing unit (31) configured to determine...
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WO/2021/125742A1 |
The present invention relates to a satellite provided with reaction wheels having a zero crossing-preventing arrangement structure and rotational direction. A purpose of the present invention is to provide a satellite provided with react...
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WO/2021/123632A1 |
The invention relates to a device for docking with a satellite, comprising: a mobile receiving platform (10) suitable for bearing against a protruding element of the satellite, a device for capturing the protruding element, and a device ...
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WO/2021/126285A1 |
Ruggedized avionics assemblies for use on kinetically launched space vehicles are disclosed. The avionic assemblies are able to maintain structural integrity and functionality under high acceleration forces generated during kinetic launc...
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WO/2021/122137A1 |
The invention relates to a device (100) for orienting a load (10) intended to orient said load about a main axis X and a secondary axis Y, comprising: - a first shaft, called transmission shaft (11), intended to support the load and conf...
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WO/2021/117105A1 |
A cooling apparatus (100) cools an electronic device (2) or other heat-generating device mounted on a satellite or other such carrier. The cooling apparatus (100) is provided with an annular refrigerant flow path (10) formed by sequentia...
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WO/2021/118401A1 |
The invention relates to rocket and aircraft technology. A device for the high-speed intercontinental transportation of passengers is configured in the form of an aircraft provided with extendable landing gear, aerodynamic control surfac...
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WO/2021/118397A1 |
The invention relates to space engineering, and more particularly to spacecraft that can be used individually or in a constellation for monitoring and warning of disasters, providing global Internet coverage and other purposes, and which...
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WO/2021/117681A1 |
A static electricity eliminating device (10) has: a first conductor (11) electrically connected to at least a part of a static electricity elimination target object 1; and a dielectric shell (15) that forms, between the shell and the fir...
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WO/2021/110489A1 |
The invention relates to a deployable structure (10) comprising a segmented structure (20) comprising N assemblies (21) of n articulated adjacent elementary panels (22), the assemblies being joined two by two by a connection panel (24). ...
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WO/2021/110841A1 |
The invention relates to a space cold gas thruster operating with a solid propellant. The cold gas thruster of the invention comprises a tank (1) suitable for containing a solid propellant and a tank (1) heating device suitable for subli...
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WO/2021/105239A1 |
The invention relates to a multi-layered garment comprising at least an inner layer, an outer layer and an intermediate layer located between said inner layer and said outer layer, wherein said intermediate layer is made from a compositi...
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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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