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Matches 1 - 50 out of 13,709

Document Document Title
WO/2019/028404A1
A satellite dispenser door release mechanism is disclosed. In various embodiments, a satellite door dispenser as disclosed herein includes a wire or cable having a first end configured to be secured in a structure comprising or coupled t...  
WO/2019/028408A1
A satellite dispenser is disclosed. In various embodiments, a satellite dispenser as disclosed herein includes a dispenser body defining an interior cavity configured to receive a payload; and a composite guide rail comprising a groove c...  
WO/2019/026179A1
A wireless communication device installed in a drone transmits information pertaining to the drone, a relay that flies at a first altitude between the altitude at which the drone can fly and the altitude of a communication satellite rece...  
WO/2019/028407A1
A satellite dispenser door assembly is disclosed. In various embodiments, a satellite dispenser door assembly as disclosed herein includes a dispenser door having a hinge pin; and a one way clutch bearing within which the hinge pin is fr...  
WO/2019/028410A1
A satellite dispenser and method of using same are disclosed. In various embodiments, a satellite dispenser as disclosed herein includes a dispenser body defining an interior cavity to accommodate a payload; and a plurality of externally...  
WO/2019/020330A1
An electric thruster comprises a propellant delivery system, wherein the propellant delivery system comprises: a pipe for carrying propellant; a valve which is adapted to adjust a volume or mass flow of the propellant in the pipe; and an...  
WO/2019/022655A1
A multiple payload set (3) for a launch vehicle, wherein the multiple payload set (3) comprising a plurality of payloads (2). The plurality of payloads is interconnected via a non-self-supported connection structure (16) before assembly ...  
WO/2019/021220A1
The present invention relates to a re-entry module comprising an alpha-dome comprising a petal structures [1-5, 49] positioned on the upper surface [7] of the base for enclosing the payload; Omega hexon positioned parallel to surface [9]...  
WO/2019/021036A1
A device which assists vertical landing of a returnable rocket stage not equipped with stabilization means during landing. The device is a structure made of mechanisms and supports which hold the stage in a vertical position during landi...  
WO/2019/020499A1
The invention relates to a method (100) for simulating the estimation of a lag in producing satellite images associated with at least one predetermined zone of the Earth (20), by at least one Earth observation satellite comprising an opt...  
WO/2019/018139A1
Artificially directing a plurality of space-borne natural bodies to a target accretion region, such that gravitational forces amongst the plurality of space-borne natural bodies within the target accretion region produces an agglomerated...  
WO/2019/018826A1
Spacecraft servicing devices or pods and related methods may include a body configured to be deployed from a host spacecraft at a location adjacent a target spacecraft and at least one spacecraft servicing component configured to perform...  
WO/2019/018001A1
A three-dimensional multi-shell insulation configured to conform to the shape of a spacecraft component to be insulated. The insulation may have a plurality of nested shell layers that are displaceable relative to each other for providin...  
WO/2019/018821A1
Spacecraft servicing devices and related methods may include a propellant tank configured to store a propellant and to be placed into fluid communication with a portion of the target spacecraft.  
WO/2019/018085A1
Cell-based systems may interlock in a reconfigurable configuration to support a mission. Space systems, for example, of a relatively large size may be assembled using an ensemble of individual "cells", which are individual space vehicles...  
WO/2019/016888A1
Provided is a terminal for displaying the surroundings of a probe vehicle, the terminal having: an operating unit that receives, from a user, the position of a target present around the probe vehicle and designation of the type of said t...  
WO/2019/017979A1
Systems, methods, and software described herein provide enhancements for orbital satellite platform. In one example, an orbital satellite platform includes a plurality of satellite devices configured to establish a pseudo-geosynchronous ...  
WO/2019/018086A1
Cell-based space systems with nested-ring structures that interlock and can change configuration to support a mission are provided. The cells may self-assemble into a larger structure to carry out a mission. Multiple rotatable rings may ...  
WO/2019/018819A1
Spacecraft servicing systems include a spacecraft servicing device and at least one pod comprising at least one spacecraft servicing component. The spacecraft servicing device is configured to transfer the at least one pod to a target sp...  
WO/2019/012755A1
[Problem] To provide a sheet-like structure which allows the sheet-like shape thereof to be estimated with a high degree of precision. [Solution] This sheet-like structure is equipped with a sheet-like member and a plurality of detection...  
WO/2019/014386A1
A system for enhancing the thrust produced by an aircraft propulsion element having a propulsion fluid outlet includes a shroud element having an inlet, an outlet and a diffusing section positioned between the shroud element inlet and sh...  
WO/2019/011919A1
The invention relates to a navigation satellite (10, 10', 10"), in particular for a medium earth orbit (MEO), having a housing (12) and a navigation antenna (16) connected to the housing (12) for emission of navigation signals in a prefe...  
WO/2019/014085A1
An apparatus is disclosed. The apparatus has a cooling fluid passage (310, 510, 810, 910), a gaseous fluid blower (315, 515, 705) disposed at an upstream portion or a downstream portion of the cooling fluid passage (310, 510, 810, 910), ...  
WO/2019/009154A1
This mobile image pickup device is provided with: an image pickup unit (20) and an acceleration/angular velocity detection unit; a processing unit that processes acceleration/angular velocity information detected by the acceleration/angu...  
WO/2019/005840A1
A wide field-of-view celestial sighting system (400) and method (500) are provided. The method (500) includes orienting an imaging optic (14, 42, 44) to collect light from at least one light source, such as at least one celestial body (1...  
WO/2019/003468A1
Provided is an aerial vehicle that prevents others from precisely measuring the position of a subject vehicle and allows friends to precisely measure the position of the subject vehicle. An aerial vehicle (10) is provided with a reflecti...  
WO/2018/234705A1
Cryogenic propellant tank (1) for a spacecraft engine, comprising an external enclosure (10) defining an internal volume, characterized in that the internal volume of the tank comprises a primary volume (V1) and a secondary volume (V2) c...  
WO/2018/231800A1
Propulsion systems that generate thrust from pressure generated by thermally decomposing a chemical blowing agent (CBA). In some embodiments, the CBA decomposes exothermically such that once thermal decomposition has been initiated, the ...  
WO/2018/231310A2
A spacecraft propulsion method uses cosmic ray triggered nuclear micro-fusion events to provide repeated or continuous thrust for artificial gravity during a space flight. In one embodiment, successive packages of deuterium-containing mi...  
WO/2018/231714A1
A high throughput fractionated satellite (HTFS) system and method where the functional capabilities of a conventional monolithic spacecraft are distributed across many small or very small satellites and a central command and relay satell...  
WO/2018/226287A1
A method, operable in the presence of ambient cosmic rays, is provided for braking a craft upon approach to a planet, moon or other space body, e.g. in preparation for landing. Deuterium-containing particle fuel material is projected in ...  
WO/2018/225688A1
Provided is a multilayer heat-insulating material which reduces a deterioration in heat-insulating performance at the periphery of a mounting means for mounting on a mounting subject and which facilitates deformation into a desired shape...  
WO/2018/224998A1
An attitude control and thrust boosting system (100) for a space launcher is disclosed, wherein the space launcher is equipped with a rocket engine (303) provided with an exhaust nozzle. The exhaust nozzle comprises a divergent portion (...  
WO/2018/224803A1
A phased array antenna and apparatus incorporating the same An electromagnetic phased array (100) is disclosed comprising a plurality of antenna elements (102), each antenna element (102) comprising at least three constituent antennae (1...  
WO/2018/220990A1
[Problem] To provide a sheet-like optical device that is capable of selectively emitting light of which the direction of the optical path is changed. [Solution] An optical device (1) is provided with a first sheet (50) and a second sheet...  
WO/2018/220699A1
A lunar orbiter system is obtained in which functions (positioning, communication, flashing) are assigned to artificial satellites in accordance with the relative positions of the artificial satellites in relation to the moon when the mo...  
WO/2018/222796A1
A satellite that includes a housing, a circuit board containing circuitry and disposed in the housing, a battery disposed in the housing and electrically connected to the circuit board, one or more weights disposed in the housing, wherei...  
WO/2018/216761A1
A robot comprises a telescoping device that can freely extend and contract in at least one direction, at least two end effectors that are respectively connected to at least two ends of the telescoping device, and a control unit that can ...  
WO/2018/210929A1
Device (52) for regulating the rate of flow of propellant fluid for an electric thruster, of the thermo-capillary device type comprising at least one capillary duct that is electrically conductive and capable of regulating the rate of fl...  
WO/2018/208201A1
A payload dispenser (1)for a launch vehicle comprising a plurality of panels (2), wherein at least one panel (2) comprises at least one payload (3) mounted onto the panel (2). The panels (2)are attachable to each other by means of attach...  
WO/2018/208193A1
A payload dispenser (1)for a launch vehiclecomprising a plurality of panels (2), wherein at least one panel (2) comprisesat least one payload (3) mounted onto the panel (2). The panels (2)are attachable to each other forming a self-suppo...  
WO/2018/209185A1
Integrated power module device, systems, and methods are provided in accordance with various embodiments. For example, some embodiments include a system that may include one or more integrated power modules. Each integrated power module ...  
WO/2018/200183A1
A satellite system can include one or more satellites that orbit the Earth. The one or more satellites may have satellite buses that support antenna arrays. The antenna arrays may include space fed arrays. Each space fed array may have a...  
WO/2018/196888A1
The invention relates to an electromagnetic toroidal impeller in the field of physics applied to electromagnetism. The invention comprises a cylindrical arrangement of superconducting antennas (9) which are separated by a dielectric (8) ...  
WO/2018/191992A1
Disclosed is a dual-axis rotation cycloid ring acceleration power device, comprising a main ring (1) connected to a motion carrier, and a secondary ring (2) movably arranged on the inner side of the main ring. The main ring and the secon...  
WO/2018/195512A1
A system for compact stowage and deployment of a flexible solar array includes a deployer unit and a blanket container for containing the flexible solar array. The deployer unit includes a frame, a closed-section collapsible mast for dep...  
WO/2018/192898A1
The subject matter of the invention is a deployable tubular structure, for protecting a piece of equipment (40) of a satellite (100), comprising a membrane (20) and a support frame of the membrane, the frame comprising a base (10a), a pl...  
WO/2018/191256A1
Methods, systems, and devices for foldable tube with unitary hinge are provided in accordance with various embodiments. Some embodiments include a device that may include one or more foldable tube sections configured to facilitate the de...  
WO/2018/189633A1
An automatic apparatus (1) for the controlled launch and recovery of a "tethered" mass (M) in orbit (or in free fall) comprising: a support structure (2) abutting on a reference surface, a winding assembly (3) coupled to the support stru...  
WO/2018/188555A1
Disclosed in the present invention is a method for reducing air resistance to a high speed moving object, comprising: first, using a multi-microporous air permeable material to prepare the housing of a moving object, such that one side o...  

Matches 1 - 50 out of 13,709