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WO/2020/214381A1 |
An apparatus includes a structure (100, 300, 700) configured to receive and transport thermal energy. The structure includes one or more materials configured to undergo a solid-solid phase transformation at a specified temperature or in ...
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WO/2020/209136A1 |
The objective of the present invention is to provide a toilet for microgravity space with which it is possible to limit electric power usage for recirculating air, using a simple configuration for a toilet bowl. A simple toilet device 10...
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WO/2020/205174A1 |
Networked initiation systems for hold-down and release mechanisms (HDRMs) are described. The systems include a control unit, a plurality of firing control units operably connected to and in communication with the control unit, wherein ea...
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WO/2020/206096A1 |
Systems, apparatuses, methods, and software are described herein that provide enhanced logistical control over spacecraft. This logistical control can include attitude adjustment and desaturation of reaction wheels. In one example, a met...
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WO/2020/201733A1 |
The present disclosure relates to a coupling assembly for fluidly connecting first and second spacecraft. The first spacecraft comprises a drive mechanism and the second spacecraft comprising a valve for filling and/or draining the secon...
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WO/2020/202221A1 |
A method for detecting and modeling objects in space using LIDAR is disclosed. The method includes transmitting a laser beam to detect at least one object in space. Further, the method includes detecting one or more data related to at le...
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WO/2020/204080A1 |
[Problem] To provide a tether and an artificial celestial body that can further reduce the burden of collision avoidance on and the risk of collision with satellites in operation or the like. [Solution] A tether 10 comprises a member in ...
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WO/2020/193926A1 |
The invention relates to a method for removing webs (2) formed on a wall (12) of a central canal (11) of a solid-propellant charge (1), characterized in that the method comprises a step (110) of removing webs (2) by shaving the wall (12)...
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WO/2020/191427A1 |
A method and system for detecting an orbiting object is disclosed. The method involves receiving a sequence of consecutive images of a region in space in which the object moves, processing the sequence of consecutive images to generate a...
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WO/2020/198177A1 |
A solar panel module has a flexible circuit board, a matrix of solar cells surface mounted thereto, a coverglass extending over the matrix of solar cells and the flexible circuit board bonded to a rigid support panel. The circuitry inclu...
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WO/2020/193916A1 |
The invention concerns a device (30) for determining an attitude of a satellite (10), the satellite comprising an attitude control system comprising a gyroscopic actuator (20) comprising a flywheel (21) mounted such that it can rotate ab...
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WO/2020/197417A1 |
Systems are described for controlling thoroughfare of a UAV through a tunnel used by primary vehicle traffic. The system interfaces with UAV flight systems and a primary vehicle data system. Data representing primary vehicle traffic timi...
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WO/2020/188207A1 |
The present invention concerns a method (50) for attitude control of a satellite (10) in low inclined orbit in survival mode, the satellite (10) comprising at least one solar generator (12), at least one solar sensor (17a, 17b), magneto-...
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WO/2020/182623A1 |
A spacecraft attitude control module (1) according to the invention is compact and easy to assemble with additional modules to form an operative attitude control system. The module comprises a robust rectangular, preferably cubic support...
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WO/2020/182682A1 |
The invention relates to an androgynous coupling means (10, 16, 17) exhibiting both male and female coupling sections (11, 12), wherein the androgynous coupling means is configured for form fit coupling with at least one further androgyn...
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WO/2020/186107A1 |
A method in a spacecraft for transporting propellant to be consumed by a thruster includes storing the propellant in the spacecraft in a solid state during at least a portion of a take-off procedure and supplying the propellant to the th...
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WO/2020/182692A2 |
The invention relates to an androgynous coupling means (10) exhibiting both male and female coupling sections, wherein the androgynous coupling means is configured for form fit coupling with at least one further androgynous coupling mean...
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WO/2020/178614A1 |
There is described a capture system (100) adapted to capture orbital objects (2000), in particular for deorbiting purposes. The capture system (110) comprises (i) a deployable capture structure (110) designed to be deployable between a s...
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WO/2020/181117A1 |
To manage propellant in a spacecraft, the method of this disclosure includes storing propellant in a tank as a mixture of liquid and gas; transferring the propellant out of the tank; converting the mixture of liquid and gas propellant in...
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WO/2020/174378A1 |
A novel cooling system for a superconducting electromagnet (740) that is suitable for use in satellite (700), or at least one or more components of the electromagnet (740) is disclosed. A satellite (700) and electromagnetic control syste...
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WO/2020/174453A1 |
An example system for controlling a target satellite includes: a satellite-control spacecraft including: a propulsion subsystem configured to propel and navigate the spacecraft proximate the target satellite; and a satellite-capture subs...
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WO/2020/173020A1 |
A flight control intelligent data analysis and decision support system for spacecraft rendezvous and docking, comprising: a flight control real-time data acquisition and processing module, a flight control simulation and verification mod...
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WO/2020/171852A1 |
Systems and methods are provided for protecting a temperature sensitive object. A system includes a temperature sensitive object and a thermal control material in thermal communication with the temperature sensitive object. The thermal c...
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WO/2020/170015A1 |
The present invention related to design of a spaceship for the space travel system. The invention is related to control of space craft or spaceship, and more particularly to systems for controlling the orientation and operation of the sp...
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WO/2020/166155A1 |
[Problem] To provide an electron source that is lightweight and simply constructed, and is capable of suppressing characteristic degradation or recovering characteristics without increasing power consumption. [Solution] This CNT electron...
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WO/2020/163825A1 |
A communication system consists of a satellite constellation including a number of NGSO satellites, one or more gateways and a control center. The satellites facilitate communication for multiple user terminals. Each gateway communicates...
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WO/2020/161434A1 |
The invention concerns a solid or liquid propellant (2) tank (1) for propellant, the tank (1) comprising means for forming a gas (9) in the tank, the tank (1) having an opening (4) of area S for extracting a flow (20) of propellant gas f...
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WO/2020/161446A1 |
The subject of the invention is computer systems (100) for acquiring satellite images. The invention also comprises devices (120) for computing satellite mission plans, and Earth-observation satellites (110). The general principle of the...
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WO/2020/155458A1 |
Provided are a flying method and a flying device. The method adopts a medium (8) and a medium acceleration unit (13) on the surface of a planet; under the action of electricity, the medium acceleration unit (13) works, and transfers the ...
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WO/2020/155460A1 |
Disclosed are a method for flight on the moon and a flight device using the method. A medium on the surface of the moon and a medium accelerating unit are adopted in the flight method. Under the action of electric power, the medium accel...
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WO/2020/158505A1 |
A satellite constellation forming system (100) forms a satellite constellation (20). The satellite constellation (20) is composed of a satellite group (300). The satellite group (300) in the satellite constellation (20) provides services...
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WO/2020/160314A1 |
Systems and method for controlling the attitude maneuvers of a spacecraft in space are provided. The method automatically generates optimal trajectories in real-time to guide a spacecraft, providing a much more robust and efficient metho...
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WO/2020/156931A1 |
The present invention relates to system for transferring a fluid from a first spacecraft to a second spacecraft, the first spacecraft comprising a fluid transfer system comprising: a pressurant supply system, a first fluid tank configure...
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WO/2020/157802A1 |
An artificial satellite (101) is provided with a monitoring device, a propulsion device, and a monitoring control device. The monitoring control device controls the propulsion device while the artificial satellite orbits the Earth (120)....
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WO/2020/158000A1 |
An artificial satellite (101) comprises a monitoring device, a propulsion device, and a monitoring control device. The monitoring control device controls the propulsion device while the artificial satellite orbits the earth (120). Thus, ...
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WO/2020/158001A1 |
This satellite constellation formation system (100) is for forming a satellite constellation (20). The satellite constellation (20) is formed from a satellite group (300). The satellite group (300) of the satellite constellation (20) pro...
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WO/2020/157807A1 |
A satellite constellation formation system (100) forms a satellite constellation (20). The satellite constellation (20) is composed of satellite groups (300). The satellite constellation (20) is configured such that the satellite groups ...
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WO/2020/152744A1 |
This spacecraft changes the orbit or orientation of a target object in outer space by irradiating the target object with a laser, the spacecraft having: a laser device for generating a laser; a focusing means for focusing the laser; a de...
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WO/2020/152747A1 |
This propulsion force enhancing member, which is to be mounted on the surface of an object present in outer space, has a transparent member transmitting an irradiated laser, and an opaque member provided between the transparent member an...
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WO/2020/150117A1 |
The Guideless Resilient Androgynous Serial Port (GRASP) mechanism provides an androgynous mechanical and electrical interface that can be tailored to the meet the requirements of a given application. Each mechanism is equipped with physi...
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WO/2020/148676A1 |
The invention concerns a method (1) for estimating the angular velocity (and, preferably, also the attitude) of a space platform (for example, a satellite, a space vehicle, or a space station) using only the information provided by one o...
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WO/2020/150242A1 |
Spacecraft servicing devices or pods and related methods may be configured to be deployed from a carrier spacecraft and include at least one spacecraft servicing component configured to perform at least one servicing operation on the tar...
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WO/2020/146013A1 |
A self-contained payload module and method of deployment of a payload includes a housing that is configured to engage a propulsive payload adapter hub, at least one deployable payload that is arranged in an interior cavity of the housing...
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WO/2020/140178A1 |
The present invention relates to the technical field of on-orbit space launching. Disclosed is an on-orbit launching apparatus. The main body of the apparatus is a permanent magnet linear synchronous motor, and the apparatus comprises a ...
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WO/2020/139102A1 |
An orbital studio module comprises a housing (1) with internal sound-proofing walls (3), solar batteries (2) and a docking device (15) with a noise-damping device (26) at a hatch (25). A large window (31) and small windows (21) are provi...
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WO/2020/139188A1 |
An ion thruster (1, 1a) and a method for providing trust is disclosed. The ion thruster (1, 1a) comprises a first electrode (3, 3a), magnetic field generating device (2, 2a) providing a magnetic trap zone (MT) at the first electrode, and...
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WO/2020/133544A1 |
A spatial micro-interference release mechanism and a locking and micro-interference release method therefor. The release mechanism comprises a force sensor beam (1), an upper top surface (2), a single guide-rail slide table (3), an inner...
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WO/2020/139101A1 |
A module having an umbrella configuration has an upper dome (1) and a lower dome (2), to which a hollow telescopic shaft (3) with a spring (6) is attached. The domes are covered on the outside with solar panels. On the lower end there is...
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WO/2020/139187A1 |
An ion thruster (1) and a method for providing trust is disclosed. The ion thruster comprises a sputtering magnetron (2), a target (3) arranged at the sputtering magnetron, and a second electrode (4). During a first pulse, the target is ...
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WO/2020/136984A1 |
In general, the hours of operation of an antenna for an orbiting satellite include much down-time. An information processing device according to the present technology is provided with a period calculation unit which, on the basis of orb...
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