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WO/2023/073557A1 |
The present invention relates to a compact release mechanism for a nanosatellite that has the purpose of holding a test mass (sphere) inside a chamber where an experiment is carried out. The test mass is held by means of two mobile walls...
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WO/2023/073319A1 |
The present invention relates to a mixed experience simulator (1), in particular a simulator of low-gravity jumps, comprising: a control unit (10); a harness (20) designed to receive a user (2) having a measurable weight; a mixed reality...
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WO/2023/071063A1 |
Provided in the present invention are a rotary test mechanism and a test method under vacuum low-temperature conditions, which relate to the technical field of spacecraft simulation tests. The test mechanism comprises a stepping motor, a...
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WO/2023/073721A1 |
An oxidizer tank is disclosed. The oxidizer tank comprises: a first shell and a second shell; and a flexible diaphragm separating the first shell from the second shell, thus defining: a first compartment, configured to contain the oxidiz...
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WO/2023/073533A1 |
The present disclosure relates to a damper device (100) configured to dissipate energy from at least one connecting cable (10) suitable for connecting a first satellite module (200) and a second satellite module (300), said damper device...
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WO/2023/069723A1 |
In one embodiment, an air-scoop includes an air inlet that air molecules enter the air¬ scoop through at an orbital speed when the air-scoop is moving through an atmosphere at the orbital speed. The air-scoop also includes a rotor that ...
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WO/2023/066753A1 |
The invention essentially consists of a heat pipe with re-entrant grooves, in which the connection channels between the liquid channels and vapour channel are open more widely in the condenser than in the other zones of the heat pipe (ev...
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WO/2023/070001A1 |
Aspects of the present disclosure relate to an extendable conductor assembly. A conductor of the extendable conductor assembly may be extended (e.g., into a thermal target, such as a preexisting or a newly created feature of a planetary ...
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WO/2023/062765A1 |
A shape/posture estimation device (50) is configured to comprise: a light intensity curve acquisition unit (54) which acquires, from a light intensity measurement device (10) for measuring light intensity of a moving body (1) to be monit...
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WO/2023/061587A1 |
The present invention describes a technology to simulate extraterrestrial conditions for investigating the effect of microgravity and CO2 rich atmosphere on animal and vegetable cells cultivation and a process thereof exploiting extrater...
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WO/2023/061155A1 |
A space station common-view time comparison orbit error correction method, comprising five parts, i.e., determination of simultaneous visual moments of two stations, calculation of projection coefficients of orbit errors, calculation of ...
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WO/2023/062731A1 |
A detection satellite (220) of a satellite constellation (200) detects launch of a flying object and transmits launch detection information to each artificial satellite on a detection orbital plane via communication with front and rear a...
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WO/2023/059219A1 |
The invention relates primarily to means for carrying out extra-vehicular activity on the surface of celestial bodies. The proposed hermetic coupling device comprises: a hermetic cabin (1); a frame (2) with an interface (3); electrically...
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WO/2023/057606A1 |
The invention relates to a rocket stage (1) for a multistage space launch vehicle (3, fig. 3), comprising a main engine (5) and being configured for stage separation from the remaining parts of the space launch vehicle (3, fig. 3) such t...
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WO/2023/059413A1 |
Electroaerodynamic devices and their methods of operation are disclosed. In one embodiment, ions are formed by dielectric barrier discharge using a time-varying voltage differential applied between a first electrode and a second electrod...
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WO/2023/054154A1 |
This satellite monitoring system (500) exchanges monitoring information (590) with a lunar/planetary exploration satellite (409) when a monitoring satellite (521) passes through the vicinity of the lunar/planetary exploration satellite (...
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WO/2023/053207A1 |
A spacecraft-borne propulsion device (1000) is characterized by a configurational form which is provided with: a propellant storing mechanism provided with a propellant storage container (10) for storing propellant in a vapor-liquid equi...
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WO/2023/052270A1 |
An Earth monitoring system comprises a satellite constellation (310) and a schedule calculation module (302) located on Earth. The schedule calculation module (302) may be configured to implement a satellite management method receiving a...
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WO/2023/049301A1 |
A weight distribution system for a protective suit includes a harness. The harness has a harness interface. The system also has a suit interface coupled to the protective suit. The system further includes a strap adjuster which adjusts t...
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WO/2023/049186A1 |
Disclosed herein is a space-based distributed radar system for facilitating imaging of areas, in accordance with some embodiments. Further, the space-based distributed radar system comprises a satellite cluster including satellites. Furt...
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WO/2023/047036A1 |
The invention relates to a scanning imaging system (1) intended to be carried on board a satellite in orbit around a planet, to capture images of portions of the planet's surface at two different inclination values of a line of sight (L)...
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WO/2023/047049A1 |
The invention relates to a device (1) for controlling the angular velocity of a decommissioned spacecraft (2) in order to facilitate operations for active removal of the spacecraft as space debris. Such a device comprises a stator (3) an...
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WO/2023/044155A1 |
A method for controlling a satellite using magnetics only, and a control system for implementing the method. The method involves assessing a current attitude of a satellite at a current time and location using magnetometry; setting a des...
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WO/2023/042251A1 |
Provided is a bulkhead structure that that shields a space facility (100) installed in outer space from external space. The bulkhead structure comprises a pressurized wall (11) that hermetically surrounds the space facility (100) such th...
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WO/2023/044162A1 |
A satellite in accordance with the present teachings has plural "thin" (i.e., panel-like) segments, which are coupled together and extendable along the in-track direction of movement of the satellite. One or more of these segments, which...
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WO/2023/043437A1 |
A coupling includes first and second housings, a valve element, and a guide link. The first housing is rotatable relative to the second housing. The first housing has helical cam slots and the second housing has linear cam tracks. The gu...
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WO/2023/038611A1 |
The invention relates to space technology and can be used in electric jet engines, as well as in vacuum-plasma apparatus. Proposed is a stationary ion/plasma engine comprising a magnetically conductive housing having mounted therein a di...
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WO/2023/037138A1 |
An electrodeless plasma thruster with close ring-shaped gas discharge chamber (1,10) can include a gas discharge chamber (1,10) close ring shaped in fluid communication with a propellant storage system (10,70). An antenna (3,30) can be p...
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WO/2023/037066A1 |
The present invention relates to a method (50) for acquiring images by a spacecraft (10) comprising an observation instrument (20) and a laser transmission module (30), said method comprising an acquisition phase (P50) for the acquisitio...
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WO/2023/037092A1 |
There is provided a vehicle (100) for protecting an entity (300) against directed-energy weapons (400), comprising: a housing; and a shield for absorbing or reflecting a laser beam, the shield, in use, extending in a plane from the housi...
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WO/2023/030632A1 |
The invention relates to an imaging system for imaging a surface on an astronomical body, such as the Earth. The imaging system such as a satellite imaging system comprises a telescope comprising at least first and second curved mirrors ...
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WO/2023/031967A1 |
The present invention relates to a modular configuration of the launch vehicle system. More specifically, it relates to the modular configuration technology developed to optimise the launch vehicle with respect to the number of engines i...
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WO/2023/032822A1 |
A flying object (500) flies in outer space from the earth towards the moon or a planet, or flies in the vicinity of the moon or planet. The flying object (500) is equipped with a positioning signal reception device. Ground stations (100)...
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WO/2023/032292A1 |
This information processing method is executed by a single processor or is executed by a plurality of processors running cooperatively, the method including: a first acquisition step for acquiring map information; a second acquisition st...
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WO/2023/034883A1 |
A factory for manufacturing useful products while orbiting is space uses concentrated solar energy, high vacuum, and the low temperatures available in a space environment. Gyroscopic forces from rotating machinery are carefully controlle...
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WO/2023/034291A2 |
The disclosed methods, systems, and kits provide the ability to deliver entire clean sheet designs from concept to first hot fire in under six weeks with instant specific impulses above 330 seconds in some of our engines. In examples, th...
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WO/2023/028500A1 |
Aspects of the present disclosure relate to a sample collection assembly for a vehicle. The sample collection assembly includes a perforated ground-engaging member of the vehicle and an associated sample collector. For example, a perfora...
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WO/2023/027892A1 |
Technology is disclosed herein for a spacecraft launch restraint and dispensing structure (100). The dispensing structure (100) has a number of trusses (110) and a central structure (104). When the trusses (110) are in a support position...
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WO/2023/025846A1 |
The present invention relates to a power conversion system for electrically-powered thrusters located on and/or inside a satellite.
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WO/2023/024968A1 |
A variable-stroke self-adaptive adjustment quasi-zero stiffness device and a parameter checking method, comprising: an integrating sphere, a target, a collimator, a pointing measuring instrument, disturbance sources, an inertia simulatio...
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WO/2023/027679A1 |
Proposed is a stationary ion/plasma engine comprising: a discharge chamber having an annular ionization and acceleration channel and a bottom with an inner seating surface for an anode, said chamber being made of an electrically insulati...
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WO/2023/025942A1 |
A reconfigurable, modular, and scalable space infrastructure which provides a large diversity of services on demand in space, comprising a master truss (101) for housing systems of the space infrastructure to provide several services thr...
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WO/2023/026011A1 |
The invention relates to a spacecraft comprising: a frame (4), an electrical device (1) supplied and/or controlled by electric cables, and an orientation system for orienting the electrical device (1), the orientation system comprising: ...
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WO/2023/027893A1 |
Technology is disclosed for a spacecraft launch restraint and dispensing structure. Stacks of spacecrafts (102) may be arranged around a central post (104). The dispensing structure has primary tie-down mechanisms (120) that axially clam...
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WO/2023/024203A1 |
The present invention relates to the technical field of spacecraft control, and relates to a sun-oriented directional solar wing driving device. According to the sun-oriented directional solar wing driving device, two gear rings are resp...
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WO/2023/026063A1 |
Spacecraft Heat Shield A deployable spacecraft atmospheric-entry heat shield (30, 40, 50, 60) is configured in a flasher pattern with a transformable polyhedral-surface. The transformable polyhedral-surface has a plurality of sectors (2,...
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WO/2023/024049A1 |
The invention relates to the technical field of ventilation apparatuses, in particular to an efficient aerospace ventilation device with a heating function. In order to solve the problem of poor air quality due to most of the existing ve...
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WO/2023/024311A1 |
Disclosed is a flexible space capsule, comprising a pneumatic apparatus, a solar power generation apparatus and a rotating apparatus. A capsule body comprises a first capsule body, a second capsule body and a third capsule body. Capsule ...
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WO/2023/021188A1 |
A detector module (100, 300, 400, 500, 600, 802, 1102, 1604, 1610, 1614) for image capture, in particular for an optoelectronic image capture system (200, 700, 800, 900, 1000, 1100) for an aircraft, such as a spacecraft, comprising a mai...
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WO/2023/012559A1 |
An aerial vehicle engine is proposed which may be powered an adjustable, vortex-based virtual aerospike engine. The vehicle may also include a combustion chamber which may be coupled to the exit nozzle. The combustion chamber may include...
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