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Matches 1 - 50 out of 13,912

Document Document Title
WO/2019/158888A1
The invention relates to a device for assembling a first part on a second part (30), said device comprising: at least two jaws (2, 6), said jaws being supported by the first part, such that the jaws can be placed in a closed position, in...  
WO/2019/160430A1
Artificial satellite "Card-Sat" comprising a frame (1), an upper cover (2) and a lower cover (3), both covers (2, 3) being fixed to the frame (1), the frame (1), the upper cover (2) and the lower cover (3) defining a substantially parale...  
WO/2019/161298A1
Exemplary embodiments described herein include innovative engagement devices. Exemplary engagement devices may include on or more tape spring systems. The tape spring system may include a continuous or segmented bi-stable tape spring. Th...  
WO/2019/156693A1
Systems, methods, and software described herein provide enhancements for managing data storage in a satellite platform. In one implementation, a satellite in a satellite platform may identify a request to store a data object in a storage...  
WO/2019/156634A1
A satellite subsystem PCB and a method for configuring a satellite subsystem PCB, the satellite subsystem PCB comprising a first planar surface; a second planar surface opposite the first planar surface; at least a first pair of connecto...  
WO/2019/157330A1
An electromagnetic energy momentum thruster has a cavity resonator and an electromagnetic radiation source for emitting an electromagnetic wave in evanescence into the cavity resonator. The electromagnetic wave produces a greater electro...  
WO/2019/155455A1
The present invention provides a space vehicle comprising an optical system having a field of view, the optical system comprising at least two optical elements spaced from one another along an optical axis of the optical system, thereby ...  
WO/2019/150873A1
The present invention comprises: a guide (101) that is provided to a first hinge shaft of a main hinge (Hm1); a guide (102) that is provided to a second hinge shaft of a side hinge (Hs11); and a deployment locking arm (200, 201, 202) tha...  
WO/2019/145663A1
The invention relates to a foldable/deployable device comprising at least four central sectors (4) each extending from a central portion (5) and forming, in a deployed state of said device, a main surface (20) in which: – each sector i...  
WO/2019/145942A1
Described hereafter is a device for the conversion of electromagnetic momentum into mechanical momentum to be used in airless environment. The device is built from rotating disk, made of non-magnetic material, on the circumference of whi...  
WO/2019/141401A1
A payload carrier assembly comprises a payload fairing (1) for protecting at least one payload (3) mounted on at least one payload carrier (20) of a launcher (2), comprising at least one separable fairing part (10, 11) that can be arrang...  
WO/2019/141925A1
The invention relates to an ejection method (100) for ejecting at least one payload such as a satellite. The ejection method comprises a step (108) of ejecting the payload from a spacecraft that is driven by a continuous propulsion force...  
WO/2019/138788A1
Provided is a deployable structure which can be compact in form while being stored before or after deployment and which does not retain fold lines. The nozzle 10 of a rocket motor 1 is constituted by a fixed nozzle 11 and a distortable n...  
WO/2019/140159A1
A satellite system operates at altitudes between 100 and 350 km relying on vehicles including a self-sustaining ion engine to counteract atmospheric drag to maintain near-constant orbit dynamics. The system operates at altitudes that are...  
WO/2019/140219A1
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...  
WO/2019/138660A1
This honeycomb sandwich panel is provided with: a honeycomb core 1; a first surface material 2 disposed on one surface of the honeycomb core 1 so as to be in close contact therewith; a second surface material 3 disposed on the other surf...  
WO/2019/140156A1
A satellite system operates at altitudes between 180 km and 350 km relying on vehicles including an engine to counteract atmospheric drag to maintain near-constant orbit dynamics. The system operates at altitudes that are substantially l...  
WO/2019/134511A1
A ground support device for aerospace engineering, and specifically, a manipulation robot for assembly tests of a space station experiment cabinet, comprising a movable lifting platform (1), an integrated monitoring system (2), a rotatin...  
WO/2019/136304A1
In one embodiment, an apparatus is attached to a feature to be deployed on a satellite. The apparatus includes a first material having an impedance, a second material coupled to the first material configured to provide a current or volta...  
WO/2019/135786A1
The present invention related generally to acquisition, transport, and archiving of space mineral resources, including the acquisition of samples for scientific investigation on Earth or on orbiting space stations. Another use of this ap...  
WO/2019/129896A1
A high-conductance thermal connector (1) comprises: - a heat-conducting band (2) comprising pyrolitic graphite layers arranged in stacks (5), each stack (5) being at least partially covered by a polyimide layer (6), an adhesive material ...  
WO/2019/128823A1
A modularized extensible space manipulator type ground experiment platform. An air bearing table (1) is located at the lower end, and can enable the experimental platform to be floated on a horizontal plane due to the anti-thrust effect ...  
WO/2019/133581A1
An air launched rocket for placing payloads in earth orbit comprising a lifting body having a cross sectional shape of an airfoil extending in a spanwise direction between a first and a second wing tip. The lifting body further comprises...  
WO/2019/125257A1
A separation device (1) for a spacecraft or launcher (1) comprising a nut (2) divided into at least two nut portions (2a, 2b, 2c) locked to each other by a locking device (3) in a locking position. A releasing device (4) is arranged to s...  
WO/2019/120205A1
An inflatable space-expanding cabin comprises an airlock module (1), a cabin core column, and a flexible housing (5). The cabin core column is arranged in the flexible housing (5). The airlock module (1) is arranged at an upper end of th...  
WO/2019/112873A1
Asteroid redirection and soft-landing systems are provided that use cosmic ray and muon-catalyzed micro-fusion. These systems include a micro-fusion propulsion system providing thrust for redirecting a small asteroid, as well as providin...  
WO/2019/112874A1
Cosmic ray and muon-catalyzed micro-fusion electrical generation provides electrical power for mining operations, including any asteroid habitats and mining equipment. The micro-fusion generator systems deploy deuterium-containing fuel m...  
WO/2019/112872A1
Asteroid redirection systems are provided that use cosmic ray and muon-catalyzed micro-fusion. These systems include a micro-fusion propulsion system providing thrust for redirecting an asteroid, as well as micro-fusion electrical genera...  
WO/2019/106595A1
The invention relates to a method for the safe release of artificial satellite in Earth orbit comprising providing an orbital transport spacecraft (1) able to move at orbital height and comprising a plurality of PODs (11) for releasing s...  
WO/2019/108272A1
An exemplary satellite includes a pair of payloads coupled to one another by a flexible boom, where the flexible boom is configured to enable easy manual engagement of the pair of payloads with an associated attachment hub, and also to p...  
WO/2019/106288A1
The invention relates to a system (10) for separating composites of a space launch vehicle, comprising non-pyrotechnic separating modules (12) distributed between the composites to be separated and a device (14) for activating the separa...  
WO/2019/104448A1
The present disclosure relates to a low mass system for releasably securing a robotic arm to a spacecraft and also securing various payloads to the robotic arm and to each other, permitting the robotic arm to be both moved from one locat...  
WO/2019/106591A1
The invention relates to a method of releasing artificial satellites into Earth's orbit comprising providing an orbital transport spacecraft (1) able to move at orbital height and comprising a cargo area (12a), hooking a plurality of sat...  
WO/2019/100297A1
Provided is a docking system, comprising a first docking assembly and a second docking assembly. The first docking assembly comprises a first mounting plate (1), a guide head (3), a multi-dimensional sliding device and a receiving unit (...  
WO/2019/094239A1
A boom and reflector assembly for a spacecraft including a telescopic boom having a plurality of tubular sections that are nested together within a base section when the boom is in a stowed position, where the base section is mounted to ...  
WO/2019/092126A1
The invention relates to a method for capturing images of the surface of the earth, installing an aerial platform (10) in a quasi-stationary position, equipped with an image acquisition system (11) with a large visual field (121) and a s...  
WO/2019/059975A3
A controllable shape memory alloy (SMA) hinge apparatus comprises multiple SMA elements to effect a first angle of rotation and a second angle of rotation between a first object and a second object. In one example, respective SMA element...  
WO/2019/093520A1
[Problem] To provide a tether which autonomously contracts from an extended state when cut, etc. [Solution] This tether 10 is a net which autonomously contracts by kinking when tension is released. The tether 10 has a length of several k...  
WO/2019/087236A1
[Purpose] To provide a reflector that can be developed in an easier way and a developed antenna and an aerospace vehicle that use the reflector. [Solution] Provided is a reflector comprising: a hub the cross section of which is formed in...  
WO/2019/083533A1
A system and method for detecting or identifying substances based on spectral response signatures is provided. The system utilizes IR imagery, singularly or stored in a database, in operative communication with a database or library of k...  
WO/2019/082989A1
Provided is a liquid behavior suppression device wherein the inside of a liquid container (100) is partitioned in a direction orthogonal to the central axis (O), liquid is held on the bottom side of the liquid container (100), and a plur...  
WO/2019/083691A1
A multi-stage traveling wave thermoacoustic engine is disclosed. A plurality of heat engine stages are formed as a toroidal spiral cascade of N stages inside a pressure vessel. Each stage feeds into the next stage such that all of the th...  
WO/2019/079137A1
A control system for a satellite comprises a power source and control system, a propulsion system having individually selectable solid fuel motors, a communication interface and an attitude determination and control system (ADCS). The AD...  
WO/2017/134689A3
An adaptable satellite bus (100, 300) is provided. The adaptable satellite bus (100, 300) includes a plurality of coupling brackets. The adaptable satellite bus (100, 300) further includes a plurality of structural panels (106-116) confi...  
WO/2019/078755A1
The invention relates to cosmonautics, and more particularly to transportation and deployment containers. A transportation and deployment container comprises a housing, an ejection mechanism, and a device for securing end doors. The hous...  
WO/2019/073167A1
The invention relates to thermal protection (18) comprising, superposed on one another in order, a metal plate, a first layer of insulating material, a layer of refractory fibres, and a second layer of insulating material, the metal plat...  
WO/2019/074317A2  
WO/2019/068649A1
- The subject matter of the invention is a deployable satellite mast consisting of an inflatable tube (1), which is stored in fan-fold form (1a) before deployment (1b) and can be deployed by filling the tube with a gas, and which compris...  
WO/2019/057630A1
The invention relates to a double-walled component of a space vehicle, comprising supporting structures (3) and a latent heat storage medium (4) between the two walls (1, 2), said component being produced by means of 3D pressure. Passive...  
WO/2019/055122A1
Operating a remote sensing vehicle 250 comprising a host bus platform 252 and a variable pitch instrument platform 254 movably coupled to the host bus platform in at least one degree of freedom. The method comprises establishing a pointi...  

Matches 1 - 50 out of 13,912