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WO/2024/019721A1 |
The invention includes engines adapted for using apparatuses and methods for instantiating chemical reactants in a nanoporous carbon powder, and further includes uses for such engines and vehicles incorporating such engines. The inventio...
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WO/2024/018092A1 |
Bolt release system for spacecraft and launcher separation systems, that comprises: a release device (1); a bolt (2) connected to the release device (1) and protruding therefrom; a first retaining means (3), with at least one end surface...
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WO/2024/019806A1 |
In some implementations, a device may obtain historical orbital data indicative of orbital movement of a set of satellites over a period of time, the set of satellites comprising at least a subset of satellites of the satellite constella...
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WO/2024/017850A1 |
A satellite radar antenna array is formed as a generally planar structure comprising a plurality of panels. Each panel comprises a plurality of antenna transmit/receive modules; each antenna transmit/receive module comprises a stack of p...
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WO/2024/016045A1 |
Disclosed herein is a method for remote monitoring, comprising determining, from event signals obtained from an event-based vision sensor, a rate of those event signals generated in response to changes associated with a specific object a...
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WO/2024/013460A1 |
A reusable orbital vehicle (14) for a space transport system (10) comprises a fuselage (22) the shape of which widens in a direction extending from the front end (24) of the reusable orbital vehicle to a rear end (26) of said fuselage (2...
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WO/2024/015975A2 |
Methods and systems are provided to enable a virtual FlatSat and distributed node architecture. The virtual platform may be or include a SaaS platform that enables multiple users to access computing nodes. The computing nodes may enable ...
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WO/2024/015232A1 |
Implementations of the disclosed subject matter provides a system having an artificial light source disposed at a distance from earth or other celestial body, where the artificial light source is configured to project one or more beams o...
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WO/2024/013698A1 |
A stage of a rocket is disclosed. The rocket stage may include: a body, and a plurality of foldable propulsion units spaced around a circumference of the body, where each propulsion unit comprises: a folding beam; at least one motor moun...
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WO/2024/015326A1 |
The current disclosure provides systems and methods of directly measuring angular velocity and angular acceleration of space objects and using the measured angular velocity and angular acceleration as inputs into new and unique algorithm...
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WO/2024/015450A2 |
A self-contained identification tag arranged to be attachable to a resident space object (RSO) comprising: a processor; an antenna, an energy gatherer arranged to gather energy from the environment; and an energy store arranged to receiv...
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WO/2024/013570A1 |
There is described a spacecraft docking system (D) for and method of capturing and coupling a target spacecraft (T) to a servicing spacecraft (S) provided with the spacecraft docking system (D), the target spacecraft (T) having a propuls...
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WO/2024/014460A1 |
There is provided a technique for achieving inter-satellite optical communication for a satellite having a limited calculation capability. One aspect of the present disclosure relates to an earth station, including: a data acquisition un...
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WO/2024/009293A1 |
Combined aerospace system is a multi-stage technology to deliver payloads to orbit and to midair. The system comprises a carrier aircraft, a tow aircraft, a towed spaceplane or a rocket plane or a glider. The carrier aircraft, coupled wi...
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WO/2024/002772A1 |
A system (1) for thermal regulation of a spacecraft (S), comprising: - a hot source (C) interface, - a radiator (10) having a thermally conductive body (11) comprising at least one radiative surface (12), - two separate single-phase cool...
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WO/2024/006680A1 |
A modular satellite apparatus (10) for testing materials in a space setting is provided. The apparatus (10) includes a lower member (101) and an upper member (102), as well as rear support members (103), medial support members (104), fro...
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WO/2024/006087A1 |
A pulsar-based timing and lateration system includes a detector system. In according with certain embodiments, the detector system includes a plurality of detectors, each one configured for detecting X-ray photons and generating output s...
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WO/2024/004355A1 |
This heat control structure comprises: a plurality of sheet-like or plate-like graphite members; a first holding member that holds the plurality of graphite members at a first end portion in the longitudinal direction of the plurality of...
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WO/2024/003013A1 |
The invention relates to a satellite comprising: a satellite body including at least one radiative surface configured to emit satellite heat to space; and an attitude determination and control 'ADCS' system for controlling an orientation...
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WO/2024/006730A1 |
Dynamic ram accelerator operation permits operation with lower acceleration, permitting launch of acceleration sensitive payloads such as crewed vehicles. Operational cost is reduced, and reliability improved, by reducing or eliminating ...
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WO/2024/004315A1 |
Provided is a heat control structure comprising a heat-insulating material, which is disposed between a housing that accommodates a heat control installed in a satellite and the heat control subject, wherein the heat-insulating material ...
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WO/2024/003483A1 |
The invention relates to improving the propulsion of a HET, RIT or GIT engine during solar eclipses and comprises, before the solar eclipse: deactivating the thrust and then disconnecting the bus supplied with power by the solar panel (T...
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WO/2023/249573A1 |
The invention is related to the radiation-proof radiation barrier, which aims to reduce the radiation that may emanate from the Sun by being inserted between the Sun and the Mars, as well as aiming to achieve a healthier life with the mo...
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WO/2023/247882A1 |
The present disclosure relates to a method for determining at least one pointing law, in a time window, for an observation instrument of at least one EO satellite (20) searching for EO space objects (50), the determination method compris...
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WO/2023/244208A1 |
A microwave plasma thrust system (MTPS) is provided with a heavy expanding gas mixture of carbon dioxide and GED as the microwave absorbing gas mixture. The thrust system is used to generate kinetic energy to propel objects such as space...
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WO/2023/242922A1 |
This navigation trajectory computation device (1) comprises an observable region computation unit (201) and a navigation trajectory computation unit (202). The observable region computation unit (201) calculates an observable range that ...
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WO/2023/241790A1 |
The invention is notably directed to an aircraft (10), which includes an aircraft structure (20), a thermal exchange system, a thermal insulation material (26), and fasteners (32, 35). The thermal exchange system includes a fluid-based c...
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WO/2023/242003A1 |
This specification relates to systems, methods and apparatus for controlling a global attitude of a satellite using machine-learning models, and the training of such machine-learning models. According to a first aspect of this specificat...
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WO/2023/244857A1 |
A thruster includes a mass source, an ejection outlet, and a channel forming an ejection path from the mass source to the ejection outlet. Multiple annular current paths form loops such that current flow along the loops is transverse to ...
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WO/2023/244860A1 |
An electrospray thruster includes an emitter including an array of tips, each tip of the array of tips being configured to emit ionic liquid, and an extractor electrode spaced from the emitter and comprising a conductive film, the conduc...
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WO/2023/239642A1 |
ThermaSat™ propulsion system uses water as a safe and non-explosive propellant, and which is unpressurized at liftoff. Utilizing solar thermal propulsion, the compact and efficient capacitor heats water to steam to produce high thrust ...
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WO/2023/230708A1 |
Provided herein is a system and associated method for use in a grapple fixture for detecting rigidization of a robotic capture interface between a grapple fixture and a robotic arm. The system includes a movable component configured to c...
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WO/2023/235745A1 |
A modular satellite testing platform system (1) having an upper (2) and a lower (3) member along with a plurality of support members (5), (6), intermediate members (4), and lower bar members (8) that are interconnected to the upper membe...
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WO/2023/233091A1 |
The invention relates to a device (1) for monitoring objects in space orbit around the Earth, the device (1) comprising a frame (2), a plate (3), at least three optical monitoring modules (4), and a power supply and control unit (5) hous...
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WO/2023/234420A1 |
A computer-implemented method for maintaining a spacecraft near an orbit comprises steps of detecting (3) that a distance from the spacecraft to the orbit is greater than a spacecraft threshold and in response, linearizing (5) dynamics o...
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WO/2023/225762A1 |
A controlled reactor comprises a reactor core thermally coupled to one or more heat pipes and an active cooling loop. A fluid may be circulated through the active cooling loop. A heat exchanger is thermally coupled to the active cooling ...
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WO/2023/228702A1 |
[Problem] There has been a problem of addressing laser leakage onto the ground during power/energy transfer from the space to the ground for use in space solar power systems (SSPS) and the like. Further, a problem of lesser charge carrie...
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WO/2023/230140A1 |
A foldable reflector with tensioned cable spoke system includes a foldable reflector. A central cone extends outward from a center of the foldable reflector. An outer reflector ring is hingedly coupled to the foldable reflector at an out...
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WO/2023/229287A1 |
A method for determining a collision candidate object for an object to be tracked is provided. The method comprises the steps of: acquiring location-related information regarding the object to be tracked at a target point in time; on the...
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WO/2023/220790A1 |
Hypergravity system comprising a mechanical shaft connected to at least one central motor designed to rotate the mechanical shaft, at least one connection arm connected to the mechanical shaft, at least one housing chamber, wherein each ...
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WO/2023/222966A1 |
The invention relates to thermoregulated space equipment (10) which comprises at least one mechanical support structure (1) comprising a first metal portion (2) for interfacing with the equipment, which first metal portion is rigidly con...
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WO/2023/223006A1 |
The present disclosure relates to a joint assembly configured to define a tubular body having a first end, a second end and a passage therebetween. The tubular body is configured for articulation between a first state in which the first ...
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WO/2023/218595A1 |
A control device 20 comprises: a processing unit 21 that identifies the incoming direction of radiation using a detector 10 that uses a scintillator; and a control unit 22 that controls a solenoid coil so that the magnetic field null poi...
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WO/2023/219710A1 |
A flow deflector for an aerial vehicle system has a flow deflector body, a clip arranged in an interior of the flow deflector body, and a spring within the clip. The flow deflector body includes a first portion at a forward end shaped to...
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WO/2023/217714A1 |
The invention relates to a propulsion stage of a launch vehicle, in particular a reusable propulsion stage, comprising a rocket body (2) having longitudinal axis (Z), wherein the propulsion stage (3) is provided with at least one jet pro...
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WO/2023/219837A1 |
Technology is disclosed herein for a power control and distribution unit, PCDU, (206) of a spacecraft that has a microcontroller (208) to control battery charging from solar arrays (104). Using a microcontroller (208) within the PCDU (20...
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WO/2023/217713A1 |
The invention relates to a propulsion stage of a launch vehicle comprising a rocket body (2, fig. 2) having a longitudinal axis (Z, fig. 1), wherein the propulsion stage (3, fig.1) is provided with at least one jet propulsion drive (36; ...
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WO/2023/220375A1 |
A technique provides a field service tool (FST) that allows customers to view and store engine performance data, including faults, in a convenient manner. The technique allows customers to gain insights into performance anomalies while p...
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WO/2023/213598A1 |
The present disclosure relates to a method (50) for generating an image using a satellite (10), wherein partial zones are processed successively and the processing of each partial zone comprises: - receiving (S51) at least two basic part...
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WO/2023/213420A1 |
The invention relates to a, preferably pumpless, pressure fed propulsion system for a spacecraft, preferably a satellite or microsatellite, the system comprising: - a propellant tank (101) for storing a propellant; - a first heat exchang...
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