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WO/2023/215664A1 |
Described herein is a power processing unit (PPU) for use with a Hall Effect Thruster (HET) and a Propellant Management Assembly (PMA) of a spacecraft. The PPU comprises an anode and ignitor supply subsystem that provides anode and ignit...
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WO/2023/215574A1 |
A method of moving a spacecraft from an initial orbit to a final orbit includes providing a spacecraft with thrusters traveling in an initial orbit that has a first RAAN. Thrusters are activated to move the spacecraft into a transfer orb...
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WO/2023/214039A1 |
The invention relates to a sensor device (SV1, SV2, SV3) for a transmission of data and/or an evaluation of downlink signals (DL(H1,T1)) transmitted by at least one satellite (S1) for a reconnaissance system (AS), wherein the satellite (...
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WO/2023/208366A1 |
The invention is notably directed to an aircraft carrier ground vehicle (10), which comprises a chassis (102), a landing platform (104), a coupling mechanism (106), and an actuation mechanism (108). The landing platform is designed to ac...
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WO/2023/212682A2 |
This invention is embodied in a system and method for transferring energy and mass (supplies) in low-gravity environments. Broadly, the preferred system comprises a launcher, a receiver, and a capsule. The capsule is used to transfer a p...
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WO/2023/208943A1 |
The present disclosure relates to a method of generating auxiliary data for controlling a satellite travelling in orbit around Earth, the method comprising: receiving tracking data for the satellite (101); applying an orbit determination...
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WO/2023/205122A1 |
Thrusters and spacecraft propulsion systems that include integrated heaters for heating a fluid propellant, and, more generally, heaters having integrated heating elements and nonlinear fluid- passageways for heating a fluid. In some emb...
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WO/2023/203970A1 |
An imaging planning system 20 comprises a planning unit 21 that plans an imaging plan for imaging a plurality of imaging points by using a plurality of artificial satellites, wherein the planning unit 21 generates one DAG by combining DA...
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WO/2023/203012A1 |
A method of determining one or more inertial properties of a spacecraft. The method comprises: receiving data collected at different points in time during operation of the spacecraft. The data includes information indicative of: the angu...
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WO/2023/198972A1 |
The invention relates to a method (100) for dimensioning a space launcher (LS), the space launcher (LS) comprising at least one module (M1, M2, M3), the at least one module (M1, M2, M3) comprising a structure (ST1, ST2, ST3), the method ...
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WO/2023/201261A1 |
Stackable satellites with a large diameter antenna that are configured to stack within each other like fully overlapping shallow bowls and to fit tightly within the area in a payload fairing. The bowl-shaped satellites allow the satellit...
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WO/2023/200567A1 |
The disclosure herein describes triggering image capture requests at ground Internet-of-Things (IoT) devices based on sensor events, and processing the image capture requests by satellites. An image capture request is received by the sat...
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WO/2023/200336A1 |
A cooperative orbital object identification system (1) is disclosed herein that comprises an identification station (4) and at least one tagged orbital object, i.e. an orbital object (3) with a retroreflecting identification tag (2) moun...
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WO/2023/195876A1 |
The invention relates to the field of aviation and cosmonautics. A high-heat tile for use in areas of a surface that are subject to high heat loads is formed in the shape of a circular cylinder of a given radius, having two parallel base...
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WO/2023/192059A1 |
A rocket motor (18) has an energetic material (22) between solid fuel (propellent, 28) and a casing (24) that surrounds the solid fuel. The energetic material is configured to be burned along with the solid fuel during normal operation o...
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WO/2023/189360A1 |
An observation assistance device 10 for assisting generation of control command information used for observation of a moving object has: a target area pseudo image generating unit 11 that generates a target area pseudo image representing...
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WO/2023/184945A1 |
Disclosed is a parachute system for planetary exploration. The parachute system (100) for planetary exploration is provided with sensors (40) and repair structures (50) on a parachute body, and the impact strength of dust particles is mo...
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WO/2023/190731A1 |
The present invention provides a locking device capable of locking a gimbal mechanism with a sufficient force and having a simpler structure than conventional locking devices.　The locking mechanism includes: a driven object-side pressi...
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WO/2023/187283A1 |
The present invention relates to a method (10) for allocating requests for observations of geographical areas (ZG) to be made to a plurality of satellites (30), the method comprising the steps of: - (S10) breaking down each geographical ...
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WO/2023/181027A1 |
A deployment system pivotably deploys panel elements between a stowed configuration and a deployed configuration. Actuator(s) associated with each pair of panel elements include a first bracket mountable to one panel element, a second br...
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WO/2023/181355A1 |
An information processing device 2X comprises a data acquisition means 32X and a maneuver detection means 33X. The data acquisition means 32X acquires time-series data that represents the position and time at which a space object having ...
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WO/2023/183167A1 |
A method for managing propellant in a spacecraft is disclosed. The method includes storing liquid propellant in a tank under an operating pressure controlled using a product of chemical decomposition of the propellant. The method may inc...
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WO/2023/181354A1 |
An information processing device 2X is provided with a data acquisition means 32X and an abnormality degree calculation means 33X. The data acquisition means 32X acquires time-series data representing the luminous intensity of a space ob...
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WO/2023/180646A1 |
The invention relates to a method (100) for controlling the orbit of a satellite, which method comprises: - determining (102) a manoeuvre plan (PMA) comprising at least one previous manoeuvre (PM1) of the previous manoeuvre plan (PPMA), ...
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WO/2023/179403A1 |
Disclosed in embodiments of the present disclosure are a capturing system and method for a spatial target. The capturing system comprises a plurality of capturing devices, a conveying device, a transmitting device, and a speed reduction ...
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WO/2023/177986A1 |
Described herein are apparatuses and methods for use therewith that can be used to remove dust and other types of particulates from a solar array of a spacecraft, a lander, a rover, or the like. Such an apparatus can include a main body ...
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WO/2023/177942A1 |
A monopropellant rocket thruster includes a thruster, a pump, a decomposition catalyst, and an igniter. The thruster housing includes a reaction chamber and a divergent nozzle. The pump, coupled to the thruster housing, is operable to pu...
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WO/2023/177228A1 |
The present invention relates to an electrical umbilical system for a space launch vehicle, using an electromagnet, the electrical umbilical system applying an electromagnetic method so as to fix an umbilical unit to a connection module ...
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WO/2023/170223A1 |
An ejection unit for a satellite comprises a housing (10) closed by a door (12-18) in which housing a guiding structure for the satellite is provided. The guiding structure comprises angle bars (50-56) and a clamping device for clamping ...
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WO/2023/172244A1 |
An electric ion propulsor and method of using is provided comprising a substrate having an inner surface and outer surface. A plurality of antennae mounted adjacent to each other on the inner surface and are enabled to transmit RF energy...
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WO/2023/170933A1 |
An extension boom (120) comprises a fiber-reinforced composite material. When the extended extension boom (120) is opened, the directions of the fibers in a first region are a first low-angle direction which forms a negative angle in the...
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WO/2023/167334A1 |
The present invention relates to: a core material that has air permeability and that has both lightweight and mechanical properties; and a skin-core structure that uses said core material. The core material according to the present inven...
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WO/2023/167335A1 |
Provided is a core material that can be smoothly manufactured with an improvement in the formation and strength of a base material and has excellent strength and lightness. The present invention provides the core material comprising a st...
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WO/2023/163817A1 |
An optical system can include a mirror that reflects incoming light to a sensor for detection. The position and/or orientation of the mirror can be controlled to reflect incoming light from different locations and/or directions. Position...
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WO/2023/161722A1 |
A space vehicle including a space vehicle body, wherein the space vehicle body includes an interior surface defining an interior of the space vehicle body and an exterior surface opposite the interior surface, and wherein at least a port...
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WO/2023/161719A1 |
Ae methhod includes providing a quantity of sheet metal, press-forming a first panel from the sheet metal to form a first stamped panel, press-forming a second panel from the sheet metal to form a second stamped panel, fixing at least on...
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WO/2023/161714A1 |
A system, including: a satellite; a first solar array (310), where the first solar array has at least a first solar panel; a second solar array (312), where the second solar array has at least a second solar panel; a boom (320) having a ...
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WO/2023/161718A1 |
A space vehicle including a body having an interior, an exterior, a first side and a second side; a first stacking pillar positioned on the exterior of the body at the first side thereof; a second stacking pillar positioned on the exteri...
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WO/2023/161712A1 |
A system having a first layer of satellites, where the first layer of satellites includes a first satellite (100a), a second satellite (100b), a third satellite (100c), and a fourth satellite (100d), where each of the first, second, thir...
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WO/2023/163617A2 |
The present method and device provide an increase in the operational efficiency of telescopes by mitigating the effect of bright, fast-moving objects on the operation of the guiding system and on the observation results of at least one t...
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WO/2023/161717A1 |
A space vehicle includes a first aluminum panel, a second aluminum panel fixed to the first aluminum panel around at least a portion of respective perimeters thereof to thereby form an enclosed structure having an interior volume, a plur...
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WO/2023/161713A1 |
A space vehicle includes a body; a stacking pillar (200a) coupled to an exterior of the body and defining a longitudinal axis, wherein the stacking pillar (200a) is configured to be removably coupled to a stacking pillar (200b) of an adj...
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WO/2023/163689A1 |
The invention relates to a star-shaped scanning method that provides multiple viewpoints using the same detector.
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WO/2023/163039A1 |
A communication planning device according to an aspect of the present disclosure comprises: an orbit prediction unit that predicts the orbit of a relay satellite that relays communication between a satellite having an optical communicati...
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WO/2023/157952A1 |
Provided is a system capable of eliminating complex functions and high-precision control which are necessary when a service satellite approaches space debris to remove the debris. A system 1 is for removing space debris C existing in out...
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WO/2023/158461A1 |
A launch system and method for orbital or suborbital air-launch of a payload involving releasably coupling a launch vehicle with a towed aircraft via an articulatable carriage to form an air-launch assembly, towing the air-launch assembl...
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WO/2023/158911A2 |
Compositions and methods for enhancing cancer therapy and the efficacy of the treatment of melanoma, particularly by blocking genomic instability, including chromothriptic genomic instability, to prevent therapy resistance by administeri...
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WO/2023/157951A1 |
Provided is a system configured so that when, for example, a service satellite approaches a non-cooperative outer-space object in order to provide an on-trajectory service or to remove debris, it is possible to obviate normally-necessary...
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WO/2023/155013A1 |
A method of manufacturing filters from regolith or 3d printing metal residues is presented, the method comprising (a) laying down a layer of particles of regolith or 3d printing metal residues into a mold; (b) closing the mold; (c) in-mo...
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WO/2023/156817A1 |
An autonomous jet platform (AJP) is designed for the takeoff and landing of flying vehicles that do not have landing gear. It is a structure consisting of a rigid double frame with jet engines arranged along the sides thereof. Within the...
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