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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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WO/2022/081830A1 |
In a method for routing communications through a constellation (100) of a plurality of CubeSats orbiting a planet and responsive to a ground controller, the ground controller determines optimal tunnels (210) that include inter-satellite ...
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WO/2022/081242A1 |
Carbide-based fuel assembly includes outer structural member of ceramic matrix composite material, the interior surface of which is lined in higher temperature regions with an insulation layer of porous refractory ceramic material. A con...
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WO/2022/077079A1 |
The present invention patent application relates to a method using real pressure, temperature and mass data obtained from real telemetry to control the mixing ratio by altering the temperature set in its tanks, wherein, for the purposes ...
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WO/2022/076101A1 |
Provided herein are various improvements to launch vehicle payload systems, such as employed to launch and deploy secondary payloads into orbit. In one example, a system includes a fairing configured to encase a payload within an envelop...
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WO/2022/074306A1 |
This invention discloses a system for detecting the path of moving objects. It comprises: - a first network of N1 telescopes which each have a field angle of M1 degrees and are orientated to cover an arc of C° in a plane P1, M1 being be...
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WO/2022/076084A2 |
Combined moderator-propellant technologies allow a dual-purpose fluid to act as both a nuclear moderator as well as a propellant in a nuclear reactor system, such as a nuclear thermal propulsion (NTP) system. By increasing the mass effic...
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WO/2022/074839A1 |
[Problem] To provide an unmanned rover which, while being compact and lightweight, has improved travel performance on uneven ground and is not readily damaged. [Solution] An unmanned rover comprising a main body part, a pair of wheels wh...
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WO/2022/071830A1 |
The invention relates to space-based information systems for comprehensive Earth monitoring. The present space-based system comprises compact and lightweight spacecraft which interact with distributed ground control centres for receiving...
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WO/2022/072430A1 |
Systems and methods for controlling satellites are provided. In one example embodiment, a computing system can obtain a request for image data. The request can be associated with a priority for acquiring the image data. The computing sys...
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WO/2022/069749A1 |
A spacecraft, for example a satellite, or a part thereof having a coating comprising a 2D material on an outer surface thereof is described. The 2D material comprises one or more elements, excluding C, N and S, in an amount of at least 5...
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WO/2022/072350A1 |
A gyroscopic roll stabilizer includes an enclosure, a flywheel assembly, and a motor. The enclosure is mounted to a gimbal for rotation about a gimbal axis and configured to maintain a below-ambient pressure. The flywheel assembly is rot...
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WO/2022/066154A1 |
Methods, systems, and devices for satellite operations are described. A system for satellite communications may include a payload, a power system, and a thermal management component. The payload may be configured to provide a service wit...
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WO/2022/065340A1 |
According to the present invention, a light-absorbing and heat-storing film is characterized by comprising a metal layer including a protrusion-and-recess-shaped object, wherein the average height of the protrusion-and-recess-shaped obje...
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WO/2022/065256A1 |
A communication satellite group (44), formed of infrastructure satellites which each fly in an earth orbit (LEO), flies, in a substantially equal arrangement, an orbit that has an orbital altitude and an orbital inclination for forming a...
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WO/2022/064721A1 |
In this invention, a second monitoring device comprises a +X+Y sensor (11S) directed to +45 degrees, a +X-Y sensor (12S) directed to -45 degrees, a -X+Y sensor (13S) directed to +135 degrees, and a -X-Y sensor (14S) directed to -135 degr...
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WO/2022/060661A1 |
A reusable modular spacecraft has a spacecraft bus structure configured to support spacecraft subsystems, at least one interchangeable housing component configured to be interchangeably received and supported by the bus structure, and a ...
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WO/2022/055795A1 |
Disclosed are devices, systems, apparatus, methods, products, and other implementations, including a method for detecting damage in a geographical area that includes receiving a first image of the geographical area, with the first image ...
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WO/2022/055673A1 |
Mining apparatuses, systems, and methods related to using a rocket engine's plume and a collection manifold to efficiently displace, collect, process, and store frozen volatiles embedded within or below a surface are disclosed. The plume...
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WO/2022/053768A1 |
The invention relates to a method for manufacturing an aerospace and/or aeronautic tubular composite part (1), said tubular composite part (1) comprising a tubular body (10) and at least one flange (22). The method comprising the followi...
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WO/2022/049332A1 |
The invention relates to a telescopic mast (100) comprising: • - coaxial segments (101_1,..., 101_N) that can be controlled from a stowed position to a deployed position, • - a set of guide systems (104, 104P) arranged between the ad...
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WO/2022/051511A1 |
A spacecraft propulsion system comprises an attitude adjustment thruster system with multiple thrusters (488a-d) receiving heated propellant via a shared thermal capacitance block (275). The thermal capacitance block (275) with integrate...
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WO/2022/047551A1 |
(57) This invention relates to a system for deploying solar panels for nanosatellites, which will find application in science, in space research, and in particular in the equipment of nanosatellites of the CubeSats type. The developed sy...
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WO/2022/049524A1 |
The planar electric motor for aerospatial use is a 100% electrical drive, consisting of a device capable of generating a thrust force on itself, regardless of the environment surrounding the same, even in a vacuum or in outer space. The ...
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WO/2022/051513A1 |
A spacecraft propulsion system comprises an attitude adjustment thruster system with multiple thrusters (488a-d) receiving heated propellant via a shared thermal capacitance block (275). The thermal capacitance block (275) receives energ...
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WO/2022/044007A1 |
The invention is an implementation of the space elevator wherein an inflatable tube is held up by the force of wind rushing through it from surface to height, in the manner of the 'inflatable dancer' used for advertisments. Since the dev...
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WO/2022/046103A1 |
Electro spray devices and methods of fabricating electro spray devices are described
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WO/2021/058356A9 |
The invention relates to an aerial transport device by means of connections with supply lines and cables for the transport of electricity, liquids and goods, at the limit of the atmospheres of the planets, in areas with low gravitational...
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WO/2022/040024A1 |
A wireless anti-static device is disclosed, including an electronic sensing circuit that measures the polarity and electrostatic potential of the subject relative to its surroundings. Ion guns of positive and negative polarities are able...
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WO/2022/039782A1 |
A missile including an upper stage and at least one lower stage is provided. The upper stage includes a primary flight computer configured to control a flight of the upper stage along a missile flight path such that, for example, it reac...
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WO/2022/040329A1 |
A propulsion method including the steps of providing a vehicle comprising a cylindrical reactor unit; conducting a nuclear fusion reaction in the cylindrical reactor unit; and deflecting a pulse of electrically charged ions from the cyli...
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WO/2022/040653A1 |
An unmanned aerial vehicle (UAV) or "drone" executes a neural network to assist with inspection, surveillance, reporting, and other missions. The drone inspection neural network may monitor, in real time, the data stream from a plurality...
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WO/2022/040146A1 |
Embodiments of the present disclosure generally relate to methods for cleaning aerospace components having oxidation, corrosion, contaminants, and/or other degradations. In one or more embodiments, a cleaning method includes positioning ...
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