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WO/2022/155717A1 |
The present invention relates to a novel form of air, land, subsea or space propulsion, achieved through the use of appropriate electromagnetic interactions. By using capacitors formed by symmetrical or asymmetrical conductors (1) and (2...
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WO/2022/159166A1 |
Polymeric electro spray emitters and related methods are generally described. In some embodiments, an emitter may be made from an ionic electro active polymer. The composition of the electro spray emitters described herein may enable the...
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WO/2022/153639A1 |
According to an aspect of the present invention, there is provided a method comprising: propelling a servicing spacecraft to an object; deploying one or more counter mass(es) away from a servicing spacecraft bus to offset the center of m...
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WO/2022/153619A1 |
According to an aspect of the present invention, there is provided a method for rendezvous with an orbiting object comprising: launching a tug and a servicer into a client orbit; separating the servicer from the tug; and docking the serv...
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WO/2022/150370A1 |
A method of in-space assembly includes: providing a roll of spooled high strength composite (HSC) boom, a robotic arm, and a printhead disposed at about an end of the robotic arm, the roll of spooled high strength composite boom feedingl...
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WO/2021/236585A9 |
An apparatus, system and method are provided for launching, deploying and moving mobility platforms used to produce a three-dimensional product using additive printing. The product, or object, is made by collecting materials in-situ at a...
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WO/2022/150492A1 |
A method of generating a momentum change in a vehicle by phase changing matter in a closed system is used to change the momentum of the vehicle without the need of a combustion system for propulsion. The method uses the multi-phase dynam...
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WO/2022/147507A1 |
A device and method for emitting an electrospray of ionized particles is disclosed, comprising a reservoir, an emitter in communication with the reservoir and having openings, wherein the openings are configured to permit release of the ...
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WO/2022/145303A1 |
The present invention addresses the problem of improving space efficiency in placement in an aircraft. A front-side battery pack 30 is installed in a spacecraft 1 having a curved outer wall 11. The front-side battery pack 30 comprises a ...
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WO/2022/146279A1 |
The present invention relates to a table (2) on which additive manufacturing is carried out; a plurality of panels (3) which are produced by the additive manufacturing method and surround a plurality of satellite elements (E) such as pay...
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WO/2022/144699A1 |
A method for the manufacture of a structural component (1) in composite material reinforced with stiffening stringers (2), defining, in use, at least part of an outer shell (3) of a vector (4) and comprising a skin (5) and a plurality of...
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WO/2022/137623A1 |
In the present invention, a first satellite (301) comprises: a first communication device (501) that communicates with a satellite flying ahead or behind in the same orbital plane; a second communication device (502) that communicates wi...
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WO/2022/137622A1 |
In a communication satellite system (10), each communication satellite (20) flying in a plane of an orbit such as an orbit (A), an orbit (B), or an orbit (C) includes an anteroposterior communication device for communicating with other c...
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WO/2022/137362A1 |
[Problem] To provide a spacecraft control system, a spacecraft control method, and a server device whereby it is possible to quickly transmit control data to a spacecraft. [Solution] In this invention, a spacecraft system includes: a plu...
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WO/2022/137411A1 |
In the present invention, a ground system (1) comprises: a reflection efficiency calculation unit (142) that calculates reflection efficiency of a mobile unit (2); a condition determination unit (143) that predicts the amount of light re...
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WO/2022/137344A1 |
This communication satellite system (10) is provided with a before-and-after communication device for each of communication satellites (20) flying on respective orbital planes of an orbit (A), an orbit (B), an orbit (C), etc., to communi...
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WO/2022/137341A1 |
This satellite constellation (110) comprises a plurality of artificial satellites that respectively fly in inclined circular orbits on six or more orbit surfaces that have a common orbit inclination angle and have north-south axes shifte...
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WO/2022/138053A1 |
This power control device is for a linear actuator 10 in a docking device 1 having a six-axis parallel link mechanism 5. A motor driver 11 for controlling the rotational speed of a motor M of the linear actuator 10 on the basis of a load...
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WO/2022/138182A1 |
The present technology relates to an artificial satellite and a ground system that make it possible to efficiently retain data within the artificial satellite. The artificial satellite comprises: an image processing unit that executes a ...
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WO/2022/138180A1 |
This technology pertains to a sensor device which enables sensor data to be efficiently stored and a data processing method therefor. The sensor device comprises: a control unit that generates feature amount data by executing a feature a...
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WO/2022/139942A1 |
Bi-modal propulsion systems and related methods are generally described. In some embodiments, a bi-modal propulsion system may employ a single propellant for both chemical thruster(s), operating at elevated pressures, and electrical thru...
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WO/2022/130407A1 |
The present invention relates to a combined launch vehicle and satellite system. More specifically relates to the satellite combined with the launch vehicle's upper stage to provide a more efficient system that includes tank separation t...
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WO/2022/132669A1 |
Systems, methods and device for payload transportation and high altitude atmospheric payload deployment. A gondola includes a frame which is configured to carry a payload, such as a rocket. The gondola includes a control system using a p...
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WO/2022/127313A1 |
The present invention discloses a high-precision angular velocity control method under short-time large-boundary interference. Orbital control information is brought into a posture control system by performing deep coupling analysis with...
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WO/2022/132335A1 |
A solar array may include a first rigid composite solar panel including solar cells secured to a first substrate. The solar array may further include a second rigid composite solar panel including solar cells secured to a second substrat...
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WO/2022/123244A1 |
The present invention relates to a system for power delivery to satellites. More particularly, the present invention relates to a method and system for providing power to orbiting satellites from ground stations on Earth using laser ligh...
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WO/2022/116955A1 |
A method for processing a double-layer structure of a spacecraft thrust chamber comprises: providing a first wall structure (1), a second wall structure (2) and ribs (4); bringing the first wall structure (1) and the second wall structur...
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WO/2022/118208A1 |
A spacecraft is equipped with a low and high thrust space propulsion system including at least one water reservoir (1) containing liquid water, a high thrust propulsion part and a low thrust propulsion part. The high thrust propulsion pa...
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WO/2022/115001A1 |
The group of inventions relates to the field of communicating visual information from outer space, preferably using a constellation of micro-class artificial Earth satellites. An artificial Earth satellite comprises a propulsion unit, an...
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WO/2022/115614A1 |
A composite material comprising a first shielding layer (210); at least one metal containing layer (208) over the first shielding layer; and a second shielding layer (206) over said at least one metal containing layer opposite of the fir...
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WO/2022/111227A1 |
A method and a system for assessing attitude stability using light sensing of an on-orbit star, comprising: step S1: after a satellite captures a star, adopting an inertial orientation attitude control mode; step S2: a satellite-borne ca...
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WO/2022/112718A1 |
A space transportation system (1) intended to be mounted on a space launcher (100) comprising a re-ignitable propulsion device (2) and orientable flaps (3) located at a second end (12) and a control unit (4), each flap (3) comprising act...
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WO/2022/104408A1 |
A plasma reactor is provided together with a method for generating kinetic energy to propel a craft. The reactor includes an inlet for plasma; a reactor core having an interior chamber and an exterior chamber, the interior chamber being ...
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WO/2022/109575A1 |
Systems and methods described herein include collapsible and deployable truss structures defining reduced volumes for compact storage.
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WO/2019/140219A9 |
Coatings and materials that are atomic oxygen resistant and have an atomically smooth surface that can reduce drag are disclosed. The coatings and materials can be used on at least a portion of a spacecraft intended to operate in harsh e...
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WO/2022/109515A1 |
A constellation of many satellites provide communication between devices such as user terminals (UTs) and ground stations that are connected to other networks, such as the Internet. A constellation management system (CMS) facilitates man...
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WO/2022/101625A1 |
UAV (400, 500, 600) systems and methods for simulation of reduced- gravity environments are disclosed. A UAV (400, 500, 600) system has an ascent vehicle (104), comprising ascent thrust means, and an aerodynamic, free fall descent UAV (1...
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WO/2022/100532A1 |
Provided is a clamp for an aerospace testing machine, comprising a bottom plate (1) and a mounting plate (2) welded to an outer wall on one side of the bottom plate (1); a servo motor (3) is connected to an outer wall at the top part of ...
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WO/2022/100531A1 |
An auxiliary propulsion device for an aerospace liquid propeller comprising a main propulsion device, a left auxiliary device (3), and a right auxiliary device (10). The main propulsion device comprises a housing (1). A thermal insulatio...
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WO/2022/102760A1 |
A communication control apparatus controls optical communication between a communication relay satellite and plural user satellites such that, when the communication relay satellite relays communication between the plural user satellites...
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WO/2022/103559A1 |
An electrical power system has a dual battery configuration that enables sufficient power supply for a spacecraft bus and a payload module being carried by the spacecraft. During a sunlight power mode, power is drawn from a solar array o...
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WO/2022/101268A1 |
The invention relates to a connecting unit (1) and a method for releasably connecting two retaining elements (2, 3), to which respective different components (19, 20) can be fastened. The connecting unit has a first retaining element (2)...
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WO/2022/101266A1 |
A link system (100) for a spacecraft (10) comprises control and communication circuitry and is configured to communicate with subsystems (12) in the spacecraft (10) independent of an on-board computer (102) and configured to manage commu...
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WO/2022/097097A1 |
Retrofittable satellite systems for an in-orbit host satellite comprising an enhancement module for adding a capability to the in-orbit host satellite, modifying the function of the in-orbit host satellite, and/or extending the function ...
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WO/2022/095599A1 |
A shape-memory alloy-driven connecting and unlocking structure comprises a housing (1), a position-limiting spring (2), a locking pin (3), a locking core rod (4), steel spheres (5), a connection rod (6), a driving spring (7), and a shape...
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WO/2022/090774A1 |
There is described a capture system (100) adapted to capture a target space object (SO), comprising a plurality of articulated arms (100A-D) configured to be deployable from a stowed configuration to a deployed configuration to perform c...
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WO/2022/089979A1 |
The invention relates to a method for planning a satellite maneuver, in particular for planning an orbital change of a satellite orbit after the completion of a mission (240), with the satellite (220) having a drive unit (150) with a gro...
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WO/2022/093590A1 |
A tracking system for a target flight vehicle includes at least two sensor nodes that are positioned at geographically diverse locations relative to a launch site from which the target flight vehicle is launched. The sensor nodes have a ...
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WO/2022/080208A1 |
Provided is a space navigating body that, while having a relatively simple configuration enabling reduction in size, makes it possible to capture an object without the need of highly accurate positioning. A space navigating body 1 is pro...
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WO/2022/081243A1 |
CERMET fuel element includes a fuel meat of consolidated ceramic fuel particles (preferably refractory-metal coated HALEU fuel kernels) and an array of axially-oriented coolant flow channels. Formation and lateral positions of coolant fl...
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