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WO/2022/036276A1 |
A deployable electromagnetic radiation antenna system for extraterrestrial deployment of an electromagnetic radiation directing surface, the deployable electromagnetic radiation antenna system comprising is provided. The deployable elect...
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WO/2022/032370A1 |
An artificial orbital ring system (AORS) is configured in the form of a ring-shaped satellite (1) placed on a circular orbit (5) at a height Ho around a natural astronomical body (2) in the plane (3) of the equator (4). The system compri...
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WO/2022/029827A1 |
An extensible mast (1) according to the present invention is characterized by being provided with a first fiber layer (2) which uses a fiber-reinforced plastic, a second fiber layer (3) which is disposed in contact with the first fiber l...
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WO/2021/225655A9 |
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...
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WO/2022/026032A1 |
A flexible solar array for extraterrestrial deployment and a method of manufacturing such a flexible solar array are disclosed. A power generating layer, a durable layer, and an ultraviolet radiation blocking layer are disposed such that...
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WO/2022/020382A1 |
A magnetohydrodynamic pump for use in pumping molten salts that improves upon existing solutions is disclosed. The magnetohydrodynamic pump utilizes a linear induction motor with a cavity lined with ceramic and an interior piece forcing ...
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WO/2022/016243A1 |
The present invention relates to a system for obtaining a compound for blocking cosmic, nuclear and electromagnetic radiation, comprising a hydrogen reservoir (110), a hydrocarbon reservoir (120), a vacuum chamber (130), a spark power so...
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WO/2022/018381A1 |
Disclosed is a method and system for detecting a target in space, based on images taken from a spacecraft such as a visual inspection satellite. The invention relates to a method for remotely detecting one or more targets (1) in space in...
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WO/2022/014694A1 |
The present invention provides a method of controlling a horizontal translational motion of a rocket without changing the posture of an aircraft and without increasing manufacturing costs or operating costs, to thus accurately execute a ...
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WO/2022/014209A1 |
[Problem] To provide an optical device which makes it possible to variously change the direction in which the radiation pressure of light acts. [Solution] This optical device extends along a reference plane, and is provided with a plural...
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WO/2022/011078A1 |
A telescope apparatus includes a telescope array comprising a plurality of telescopes each having a telescope aperture configured to receive light from a respective field of view. A light sensor is associated with each telescope to recei...
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WO/2022/010485A1 |
A spacecraft propulsion system including a first thruster system including a first power processing unit (30) connected to a first thruster string (20) via a crossover switching unit (40) and connected to a second thruster string (20) vi...
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WO/2022/008386A1 |
Disclosed is a primary structure (100) for a spacecraft (200), comprising an interface ring (10) and a predetermined number of panels defining a box arranged so as to close an interior volume of the spacecraft, the box being connected to...
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WO/2022/010819A1 |
A satellite used in a multi-satellite LEO/VLEO constellation is configured to reduce drag and increase satellite life in orbit by virtue of its streamlined casing. The satellite has a longitudinal axis defining the y-axis of a right-hand...
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WO/2022/004040A1 |
A system for controlling an operation of a vehicle to rendezvous with a target over a finite time horizon, wherein the vehicle and the target form a multi- object celestial system. A processor to formulate passive unsafe regions as passi...
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WO/2022/003284A1 |
The present invention relates to a method (50) for orbit control of a satellite (10) orbiting Earth and desaturation of a device for storing kinematic momentum of the satellite, the satellite (10) comprising two articulated arms (20, 21)...
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WO/2022/004044A1 |
Systems and methods controlling an operation of a vehicle in real time to rendezvous the vehicle with a target over a finite time horizon having multiple specified time periods. Select a set of unsafe regions from stored unsafe regions, ...
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WO/2021/262867A1 |
A method for orbital collision screening comprising, obtaining trajectory information of a plurality of objects moving on predictable paths. For each one of the plurality of objects, based upon respective trajectory information of the on...
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WO/2021/254547A1 |
A supporting structure for vertical transport comprising an anchoring segment mounted on the ground, a trunk of passive and compensation segments that are provided with containers with a lifting gas, wherein the lifting power of the lift...
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WO/2021/258060A1 |
A closed-loop, bioregenerative water purification system including a gravity-independent anaerobic membrane bioreactor capable of operating in the presence and absence of gravity, the bioreactor including an anaerobic bioreactor, a first...
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WO/2021/255444A2 |
A device for protecting a body from damage. The protective device comprises an outer protective cover, the outer protective cover comprising a thermal energy conduction element for transferring thermal energy through at least part of the...
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WO/2021/257002A1 |
The subject-matter of invention is a spacecraft powered by electromagnetic waves with a primary and secondary tunnel for acceleration in the interplanetary, interstellar and intergalactic space and generation of electricity to power the ...
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WO/2021/255920A1 |
The present invention enables an image-capturing plan in which changes have been reflected to be swiftly created. An image-capturing plan creating device according to the present invention comprises: an image-capturing plan creating unit...
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WO/2021/242302A1 |
Systems, methods, devices, and non-transitory media of the various embodiments may enable the identification of launch opportunities. The integrated approach of the various embodiments leverages instrumentation, data and communication sy...
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WO/2021/240487A1 |
The invention relates to a method (100) for adjusting the path of a satellite (10) to limit a risk of collision with items of debris (d1, di) each having a date of closest pass (TCA1, TCAi) with the satellite (10), the method (100) compr...
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WO/2021/243244A1 |
A nuclear fuel assembly for a nuclear reactor core, the fuel assembly having at least one fuel element including an elongated shell defining an interior volume, a lattice structure disposed within the interior volume, at least one flow c...
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WO/2021/241365A1 |
This space debris orbit changing method comprises: a step for observing space debris floating in outer space; and a step for irradiating the observed space debris with solar light condensed by an irradiation satellite provided in outer s...
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WO/2021/240404A1 |
A release system (1) for the release of satellites from a launch vehicle comprising: (i) a torsion bar (2), having a first end (2a) which is fixed by means of support means (4) to a launch vehicle (3) and is locked in rotation around a l...
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WO/2021/239732A1 |
The invention relates to a method (100) for estimating collision between a satellite (10) in orbit and at least one piece of space debris (d1) having a time of closest approach (TCA)) to the satellite (10), the method (100) comprising th...
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WO/2021/235487A1 |
Provided is a space debris removal method comprising a step for putting, on a ballistic trajectory, a space debris removal device capable of spraying liquid hydrogen or an ionic liquid, and a step for spraying the liquid hydrogen or the ...
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WO/2021/234246A1 |
The invention proposes a device (1) for deploying and pointing an item of equipment, comprising: - a mobile platform (20) for receiving the item of equipment, - a carrier (10) rigidly attached to a wall of a spacecraft, and - three ident...
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WO/2021/234054A1 |
The invention relates to a method for transferring a spacecraft (10), such as an artificial satellite, from an initial elliptical orbit (30) to a final geostationary orbit (50), said spacecraft taking at least one intermediate elliptical...
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WO/2021/229178A1 |
The invention relates to a deployment device (1) for a nano-satellite (5) comprising a main structure (2) mounted on a launcher, a support frame (3) carrying the nano-satellite (5), a locking/unlocking structure (4), the deployment devic...
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WO/2021/230170A1 |
A database (102) of a rocket launch assistance device stores orbital prediction information about a satellite megaconstellation (301) acquired from a space information recorder provided in a megaconstellation operations device, and space...
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WO/2021/226810A1 |
An optical pressure principle-based micro-thrust and micro-impulse applying apparatus and method. A micro-thrust can be produced for a target by the action of optical pressure of laser light reflection. The apparatus comprises a laser (1...
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WO/2021/230986A1 |
A method of roll steering of a spacecraft to align an aspect of the spacecraft, such as the surface of solar arrays carried by the spacecraft, to the sun, is described. The roll steering occurs only when the sun is at an angle relative t...
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WO/2021/230171A1 |
A space traffic management device (100) implemented in a megaconstellation operations device (41) determines one or a plurality of representative satellites belonging to a megaconstellation of satellites flying in orbits having the same ...
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WO/2021/232032A2 |
An antenna system is configured for use in Low Earth Orbit (LEO) around Earth. The system has a plurality of antenna satellites coupled together to form a phased array. Each of the plurality of antenna satellites have an antenna body wit...
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WO/2021/229168A1 |
The present invention relates to a method (50) for orbit control of a satellite (10) in Earth orbit and for desaturating an angular momentum storage device of the satellite, the satellite (10) comprising an articulated arm (21) designed ...
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WO/2021/230166A1 |
This space information recorder (100) has set up therein a plurality of categories selected from among: a category, for multiple different constellations, having been acquired from a megaconstellation operation apparatus and formed at ne...
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WO/2021/230169A1 |
In a space traffic management system (500), space traffic management devices (100) respectively implemented in each of a plurality of megaconstellation operations devices and a debris removal operations device (45) are connected via a co...
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WO/2021/230167A1 |
An orbital analysis unit (431) of a collision avoidance assistance operations device analyzes the orbit of a specific space object. In a case where the specific space object is predicted to intrude into the orbital altitude region where ...
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WO/2021/230168A1 |
An orbit analysis unit (431) of this collision avoidance assistance project device identifies a mega-constellation satellite group that is formed at an orbital altitude that is expected to be passed during flight of a space object operat...
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WO/2021/225701A1 |
Vehicle capture assemblies and related devices, systems, and methods include one or more probe assemblies for passively engaging with and securing the target vehicle.
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WO/2021/225621A1 |
A thrust generator is provided for producing thrust to move a spacecraft. The thrust generator includes a housing having a first end and an opposing second end. The first end is associated with a mount for coupling to the spacecraft. The...
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WO/2021/225620A1 |
A propulsion system for a spacecraft includes a thrust generator for producing thrust to move the spacecraft. A propellant storage unit is in fluid communication with the thrust generator. A control assembly is in communication with the ...
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WO/2021/225702A1 |
Vehicle capture assemblies and related devices, systems, and methods include one or more probe assemblies for engaging with and securing the target vehicle. The one or more probe assemblies may include one or more attenuation features or...
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WO/2021/225622A1 |
A control assembly for a spacecraft includes a propellant management assembly configured to adjust a supply of propellant from a storage unit to a thrust generator. The control assembly further includes a controller having a processor co...
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WO/2021/221767A2 |
A satellite propulsion system and methods of operating the same include a first ionization stage and a second acceleration stage. The first ionization stage has a plasma source configured to produce an arc discharge and emit a preliminar...
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WO/2021/221035A1 |
A Space Situational Awareness (SSA) business device (47) is a business device (40) with which an SSA business operator manages space object information. The SSA business device (47) is provided with a space traffic management device (200...
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