| Document |
Document Title |
|
WO/2021/175903A1 |
The invention relates to a method for producing a satellite (10) to facilitate the inclusion of one or a plurality of reflector antennas on a surface (11) of the satellite. A reusable generic configuration is determined in advance separa...
|
|
WO/2021/170931A1 |
The application proposes a radiator (1) for a geostationary satellite (2), comprising: - a radiating panel (4) perpendicular to a radiation axis (S), and pivoting relative to the radiation axis (S), - a support leg (7) for the panel, - a...
|
|
WO/2021/173229A1 |
Exemplary embodiments provided herein include connection systems in which a gripper is actuated through introduction of a material to an interior cavity. Embodiments may include more than one cavity such that deployment and actuation may...
|
|
WO/2021/171781A1 |
The purpose of the present invention is to provide an observation control device, an observation system, a spacecraft, an observation control method, and an observation control program which enable stable observation. An observation cont...
|
|
WO/2021/171409A1 |
In an orbital attitude control device (1150): an ideal thrust axis direction calculation unit (1505) calculates an ideal thrust axis direction on the basis of information about a preset orbit; an ideal attitude calculation unit (1506) ca...
|
|
WO/2021/172182A1 |
This satellite constellation (100) comprises a plurality of artificial satellites (111-116) in a number that is a multiple of six. Each of the plurality of artificial satellites makes a plurality of revolutions along an inclined circular...
|
|
WO/2021/166876A1 |
The purpose of the present invention is to prevent satellites constituting a mega constellation from staying in a large number in outer space, after completing the mission. A satellite is equipped with a propulsion device. The satellite ...
|
|
WO/2021/161873A1 |
This propulsion device comprises a gas generator and a plurality of thrusters. The gas generator generates combustion gas when a flying object satisfies emergency conditions. Here, the plurality of thrusters output the combustion gas dow...
|
|
WO/2021/162114A1 |
The present invention provides a production method and a production system of extracellular vesicles having a better effect than conventional products, said extracellular vesicles being usable in regenerative medicine and immune cell the...
|
|
WO/2021/157567A1 |
Provided are a spacecraft liquid propulsion system failure diagnosis system that can reliably diagnose a failure of a spacecraft, and a spacecraft liquid propulsion system failure diagnosis method. The spacecraft liquid propulsion system...
|
|
WO/2021/157568A1 |
A computer system of the present invention comprises a processor unit, and is configured to be capable of communicating with a user device operated by a first user and a satellite. The satellite includes a religious object and an informa...
|
|
WO/2021/158278A1 |
A multi-user satellite system provides communication services to external satellites. This satellite system provides in-orbit access points that can be used by the external satellites to offload data instead on relying directly on ground...
|
|
WO/2021/158417A1 |
An aerospace vehicle system, preferably including one or more capsules, and optionally including one or more propulsion modules and/ or safety modules. A capsule, preferably including a pressure vessel including a structural frame and on...
|
|
WO/2021/151732A1 |
A description is given of an actuator module (100; 200; 300; 400) for releasing an equipment component, for example a satellite or a rocket, comprising a module base, which forms a guiding sleeve (4; 304), comprising a releasing element ...
|
|
WO/2021/154124A1 |
The invention relates to electric propulsion systems for small spacecraft. The present system comprises rigid structural elements of a module, at least three gas discharge chambers, at least three antennae, at least three rings made of a...
|
|
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...
|
|
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...
|
|
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 ...
|
|
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 ...
|
|
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...
|
|
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...
|
|
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...
|
|
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...
|
|
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...
|
|
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...
|
|
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...
|
|
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...
|
|
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...
|
|
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...
|
|
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...
|
|
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. ...
|
|
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...
|
|
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...
|
|
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...
|
|
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...
|
|
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 ...
|
|
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...
|
|
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...
|
|
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...
|
|
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...
|
|
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 ...
|
|
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...
|
|
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...
|
|
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...
|
|
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...
|
|
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...
|
|
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...
|
|
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). ...
|
|
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...
|
|
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...
|
