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WO/2022/230560A1 |
A monitoring satellite (110), which has detected significantly high brightness, indicates emission time corresponding to the detection time, an emission coordinate value indicating the position where the significantly high brightness has...
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WO/2022/229185A1 |
The invention relates to a motor comprising a rotor rotating about an axis of rotation, at least two rockers articulated about a shaft attached to the rotor and centred about an axis separate from the axis of rotation of the rotor, at le...
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WO/2022/229537A1 |
The invention relates to a thermoregulated thermomechanical structure (10) for a focal plane (100) suitable for operating in a space environment, comprising an interface (17) for supporting dissipative electronic equipment, said structur...
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WO/2022/222807A1 |
Disclosed in the present utility model is a novel object propulsion apparatus, comprising a propulsion apparatus, the propulsion apparatus comprising a thermal insulation cover, and the thermal insulation cover being used for keeping an ...
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WO/2022/209149A1 |
One problem associated with conventional satellite systems is the difficulty in reducing size and weight of a satellite. A position measurement method according to the present invention includes: observing, in a first satellite (11), pha...
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WO/2022/125264A9 |
A method includes producing an electric propulsion (EP) rocket engine. The method selects a core discharge chamber. A discharge cathode assembly (DCA) is selected along with a DCA common interface (CI). The DCA CI is connected to the cor...
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WO/2022/208794A1 |
Provided is a heat insulation structure (100) provided with a heat insulation film (200) and a plurality of support members (300) for supporting the heat insulation film (200), the heat insulation structure being characterized in that: t...
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WO/2022/207558A1 |
The invention relates to a spacecraft membrane (2) which is self-supporting and flexible. The spacecraft membrane (2) has a substrate (5) made of a fluoropolymer. Furthermore, the spacecraft membrane (2) has a silicon oxide layer (6; 7)....
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WO/2022/199886A1 |
The invention relates to an atmosphere reentry and landing device (1) for a rocket stage (2) for the safe reentry of a rocket stage (2) into the atmosphere and/or the safe landing of a rocket stage (2) in water. The invention also relate...
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WO/2022/200714A1 |
The invention relates to a transport system (1) intended to be installed on a space launcher (100, figure 1) and comprising: • - an aircraft (2) which comprises propulsion means configured to propel the aircraft (2) in a direction of f...
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WO/2022/200596A1 |
An innovative landing system for a spacecraft according to the invention comprises a foldable tether-based carrier structure that when unfolded assumes wheel-type shape and in its centre supports a carrier platform for the payload of the...
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WO/2022/200713A1 |
The invention relates to a hypersonic transport system (1) comprising: - an aircraft (2) with a hypersonic lift-to-drag ratio greater than or equal to 2.5, the aircraft (2) comprising a secondary propulsion device (21) and position senso...
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WO/2022/200189A1 |
A fluid pump for generating a fluid stream (55) is provided. The fluid pump includes a first actuator (20) with a first vibration element, a second actuator (30) with a second vibration element, and a power source that is connected to th...
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WO/2022/204247A1 |
A self-deployable array of panels includes a plurality of panels, each panel having a first compressed panel thickness state and a second expanded panel thickness state, and including a spring bias element biased to the second expanded p...
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WO/2022/195137A1 |
Docking system (1) for spacecraft, comprising an end ring (3) and a docking assembly (2), the docking assembly (2) comprising: - a support ring (4) connected to a plurality of linear actuators (6) for deployment and retracting, and - at ...
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WO/2022/197797A1 |
A spacecraft has a flat antenna array having an edge and a middle portion. A reconfigurable reaction-momentum wheel is coupled to the antenna array to roll and/or pitch the antenna array in small magnitudes. The reconfigurable reaction-m...
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WO/2022/195231A1 |
The present invention relates to a system for detecting the path of moving objects, characterized in that it comprises telescopes (1-4) rotating in an azimuthal plane and each oriented with a height comprised between 30° and 85°, each ...
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WO/2022/192735A1 |
The present disclosure provides a satellite system with orbital debris avoidance. In one embodiment, the satellite system includes debris sensor circuitry to scan orbital debris items in an orbital debris field; and sensor controller cir...
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WO/2022/192424A1 |
A system and apparatuses for breaking down and collecting asteroids. The asteroid miner apparatus comprises a body, an aperture, a plurality of holes, a plurality of speakers, a drill, an attachment piece, a fan, a baggage, and a set of ...
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WO/2022/187081A1 |
A resource orchestration system includes a plurality of rechargeable devices each comprising a rechargeable power storage unit, a resource manager, and a service unit, wherein the resource manager prepares a device report for the recharg...
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WO/2022/182904A1 |
Pneumatically supported towers for low gravity applications are disclosed herein. In one aspect, an inflatable tower for use in vacuum environments can have a membrane configured to support a load when inflated with an inflation gas to a...
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WO/2022/180281A1 |
Disclosed is a retaining and releasing device for spaceships, designed to retain and release a body (M) that is releasable with respect to a support structure (F), the device comprising: a releasing bolt (1) designed to keep the releasab...
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WO/2022/179204A1 |
A carbon fiber composite truss rib and a manufacturing method therefor; the carbon fiber composite truss rib (1) has a hollowed-out grid-like and elongated plate-like structure; a circumferential rib (3) is provided on the periphery of t...
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WO/2022/176891A1 |
A monitoring system (404) includes a plurality of monitoring satellites (307), and a monitoring ground center (810). A satellite information transmitting system (403) includes a plurality of communication satellites each equipped with a ...
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WO/2022/176734A1 |
A flying object (109) flies around the Earth. Three or more monitoring satellites (120) monitor Earth's circumference from different latitudes at a time of interest, and transmit three or more sets of monitoring data. A ground system (13...
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WO/2022/176890A1 |
Monitoring satellites (100) of a monitoring system (310) monitor a flying object (520) and transmit the flying object information generated thereby to a handling system (330) via communication satellites (200) of a communication system. ...
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WO/2022/178115A1 |
A system can include an emitter structure connected to a reservoir containing a working material, wherein the working material is in electrical communication with a first electrode, an electrode opposing the emitter structure across a ga...
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WO/2022/176733A1 |
A flying body (109) flies through the Earth limb. Three monitoring satellites (120) monitor the Earth limb from differing latitudes at a target time, and transmit three sets of monitoring data. A terrestrial system (130) receives the thr...
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WO/2022/176892A1 |
In a flying object handling system (1000), a monitoring ground center (311) transmits: an ID, time information, and position information related to a monitoring satellite (100) that transmits flying object information; an ID, time inform...
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WO/2022/176889A1 |
A monitoring system (404) has a plurality of monitoring satellites each equipped with a monitoring device and a communication device. A satellite information transmission system (403) has a plurality of communication satellites each equi...
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WO/2022/176893A1 |
Provided is a method for using a monitoring system and a communication system to detect the launch of a flying object and transmit flying object information to a handling system in quasi-real-time. A plurality of satellite constellatio...
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WO/2022/176894A1 |
Provided is a flight path prediction method for highly accurately predicting the flight path of a glide vehicle. A model database (350) stores a plurality of flight path models. A ground system (340) references the model database (350) w...
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WO/2022/176895A1 |
The purpose of the present invention is to provide a communication route searching method for quickly and accurately searching for a communication route for transmitting projectile information detected by a surveillance satellite. In a c...
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WO/2022/171588A1 |
The invention describes a boom system (100) for a satellite, comprising a boom (2) which is wound up in several layers in a wound-up state and is unwound in an unwound state, wherein the boom (2) is designed to assume a predetermined sha...
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WO/2022/109747A9 |
A satellite with deployable optics is provided. The satellite has a frame, an optical axis, and a deployable optical system. The optical system has a mechanical aperture perpendicular to the optical axis, where light collected travels su...
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WO/2022/167539A1 |
The invention relates to a launch vehicle comprising a rocket body (2; 102) that has a longitudinal axis (Z, Z'), which rocket body has at least one propulsion stage (3; 103) that can be propelled by a jet propulsion means (36; 136) that...
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WO/2022/168319A1 |
An extension boom (120) is extended from a state in which the extension boom (120) is wound into a tubular shape in an extension direction coinciding with one side in the widthwise direction of the tubular shape. Protruding portions (125...
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WO/2022/163804A1 |
Provided is a mirror support mechanism capable of alleviating deformation caused by compressive force or tensile force occurring in a support member. This mirror support mechanism supports a reflection mirror 1 which has a supported pa...
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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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