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Matches 1 - 50 out of 13,538

Document Document Title
WO/2018/167473A1
The present subject matter relates to a system and a method for galactic transportation (100). The galactic transportation system (100) may comprise multiple rails (102) arranged in a first direction (103), a platform (108) for supportin...  
WO/2018/167840A1
The present invention is configured such that, for each RSO(n), in each combination of observation-possible time periods OT(h) for a number R(n) of requested observations, an evaluation value E(m,n,h) is integrated that was calculated by...  
WO/2018/167161A1
The invention relates to a method for determining, by reanalysis, a vibratory environment of a coupled vehicle/passenger system, the vehicle being subjected to external forces Fext and being coupled to a new passenger comprising x=l, ......  
WO/2018/162831A1
An electrodynamic assembly (3) for propelling a spacecraft (1) in orbit around a star having a magnetic field, comprising at least one coaxial cable (7) comprising an electrically conductive core (8) surrounded by a first electrically in...  
WO/2018/164426A1
The present invention relates to a method for detecting a porphyry copper ore body by using hyperspectral imaging of malachite, the method comprising the steps of: obtaining hyperspectral image data of an alteration zone indicated by alt...  
WO/2018/160215A1
This invention relates to magnetic propulsion systems. Previously, motors required electronic control systems for efficiency. Embodiments of the present invention use a first axel (120) joined to a first permanent magnet (113) of a first...  
WO/2018/158531A1
The invention relates to a device and a method for the connection and linear separation of two elements (1, 2), such as the two stages of a spacecraft, consisting in using a tube (4) containing a pyrogenic-type material (5) and a glue (3...  
WO/2018/160740A1
A three-axis spacecraft including a spacecraft body including first and second opposing radiator/equipment panels, first and second opposing mounting panels, an earth deck and a zenith deck. The zenith deck faces the Earth when the space...  
WO/2018/158746A1
The present disclosure relates launch systems, launch vehicles for use with the launch system, and methods of launching articles utilizing the launch vehicle and/or the launch system. In particular, various improvements for electroantima...  
WO/2018/157176A1
Transfer of objects between spacecraft can be achieved in a low gravity environment. A capture device can be part of a module that facilitates visualization of a vessel that approaches the capture device. The module can facilitate positi...  
WO/2018/157061A1
A tape drive comprises a roll of a tape (202) that can be extended from a rolled state to an extended state. The tape includes a rigid material that supports the tape and a pliable material disposed at least partially on one side of the ...  
WO/2018/154603A1
The present subject matter relates to an apparatus (100) that use of a tuft of numerous wires as a drag enhancing system for spacecrafts (102). When these ultra-thin wires are used in high numbers and deployed on-board a spacecraft, they...  
WO/2018/150883A1
Provided is a capturing system for capturing an object to be captured in outer space, wherein the success rate of missions is increased at low costs. This capturing system 1 for capturing an object T to be captured in outer space compris...  
WO/2018/147760A1
The invention relates to spacecraft of the platform type, developed in accordance with the CubeSat standard. The present spacecraft comprises a body in the shape of a parallelepiped and consisting of an upper panel and side panels, faste...  
WO/2018/147925A1
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/2018/146220A1
The invention relates to a small satellite (10) which is capable of formation flying, in particular a nanosatellite or picosatellite with a mass weight of 10 kg or less, for LEO applications, comprising a housing (12) and at least one in...  
WO/2018/138112A1
The invention relates to a flying craft (8, 98, 298, 308, 318) comprising lighter than air gas in a receptacle for creating a lifting force by means of buoyancy and a thrust force by combustion in combustion engine as a fuel together wit...  
WO/2018/139357A1
[Problem] To provide a spatial optical communication device that can transmit uplink light waves with high accuracy without the use of a laser guide star by measuring and compensating for variations in the atmosphere. [Solution] The pres...  
WO/2018/135020A1
Provided are: a lightweight, space-saving metal seamless container that can be mounted to a space rocket, wherein a metal container body having a convex surface shape such as a spherical shape is seamless, and the container body and a po...  
WO/2018/135118A1
A space debris capturing device (3) comprising a harpoon (31, 41, 41') which is driven into target debris (X) that is a piece of space debris to be removed. The harpoon (31, 41, 41') is provided with a first harpoon portion (43) having a...  
WO/2018/130754A1
The invention relates to a method for preparing a surface (2) of a cryogenic tank (1) of a space launch vehicle, the tank (1) consisting of at least one wall (2) made of an aluminium alloy, in which at least part of the surface of the wa...  
WO/2018/132036A1
The inventions relate to methods for setting different vehicles, inter alia spacecraft, into motion and to propulsion units for same. The invention proposes generating an axial driving force by accelerating a working fluid, i.e. a fluid ...  
WO/2018/127603A1
The invention relates to a transport carrier system (1), having at least one elongate take-off and landing ramp (2) and at least one flying object (3), which is designed to take off and land on the take-off and landing ramp (2), wherein ...  
WO/2018/123885A1
A spacecraft, provided with: an engine; a thrust direction control device for controlling the thrust direction, which is the direction of thrust acting on the spacecraft; and a main control device for acquiring a state quantity for the s...  
WO/2018/125333A2
A software-defined receiver (SDR) using real long term evolution (LTE) signals may be used for navigation. The LTE SDR leverages the structure of the downlink LTE signal, and provides signal acquisition, navigation-relevant high-level sy...  
WO/2018/125942A1
Methods and systems for vertically landing space vehicles are described herein. In one embodiment, a reusable space vehicle lands in a vertical, nose-up orientation by engaging a system of cables suspended from an elevated framework duri...  
WO/2018/122413A1
The invention relates to a container for receiving, storing, and dispensing liquids and/or viscous substances, in particular fuel, propellant, or drinking water, comprising a casing (12) with a microscopic surface structure (16) that is ...  
WO/2018/116490A1
A first deployment mechanism (30) deploys a first radiator panel (20) from a state in which the first radiator panel (20) faces the south surface or north surface (10) of a satellite body structure. With the first radiator panel (20) fac...  
WO/2018/118042A1
Provided herein are various improvements to satellite or payload deployment systems and equipment. In one example, a satellite deployment apparatus is provided. The satellite deployment apparatus includes opposing retention members confi...  
WO/2018/115540A1
The invention relates to a connection/separation device (1) for separating satellites from shuttles or satellite dispensers, which comprises: a plurality of clamps (2, 2') aligned circumferentially and couplable by the internal face ther...  
WO/2018/112723A1
A light source energy boosting system, comprising a reflection propelling unit (120, 220), a light source power unit (110, 210) and a feedback device (140, 240), and characterized in that: the light source power unit (110, 210) comprises...  
WO/2018/115180A1
The present invention relates to a nano-satellite bus, characterized in that it comprises: -a mono-bloc mechanical frame (1) comprising a plurality of posts and edges (2, 2') forming the sides of the said mechanical frame; -a back panel ...  
WO/2018/112637A1
The present disclosure relates to a mechanism for releasably securing components of a spacecraft together during launch until such time as the mechanism is commanded to release those components. Upon command, the components are then rele...  
WO/2018/109695A2
The present disclosure relates to a launch system and method. The launch system and method can include at least a preliminary accelerator tube system (PAT) that can be combined with a main accelerator tube system (MAT). The PAT alone or ...  
WO/2018/108905A1
The invention relates to a method and to a device for position control of a spacecraft (1). In the method, a force is exerted on the spacecraft (1) by emitting at least one directed beam (7) of electromagnetic radiation having sufficient...  
WO/2018/104521A1
The invention concerns a method for gauging the liquid propellant tank (10) of a spacecraft during a phase of high-thrust along an axis (12), said tank being thermally conductive and having a known geometry. The method comprises steps of...  
WO/2018/103762A1
A distributed propulsion system, wherein an input end of a gas collection device of a high energy working medium collection device is connected to an output end of a core machine gas compressor of a turbine engine core machine, an output...  
WO/2018/100274A1
A system for correcting POGO effect for a system for supplying liquid propellant to a rocket engine, comprising a liquid propellant supply line portion (70), a hydraulic accumulator (11), comprising a tank (12) connected to the supply li...  
WO/2018/096236A1
Device and method for regulating a flow rate of gas intended to supply a propulsion apparatus for a spacecraft comprising xenon tank (2), a circuit comprising a withdrawing pipe (3) having an upstream end connected to the tank (2) and a ...  
WO/2018/096244A1
The invention relates to a system for correcting pogo oscillation for a system for supplying liquid propellent to a rocket engine, comprising a supply duct portion (70) for supplying liquid propellent, a hydraulic accumulator (11), compr...  
WO/2018/094504A1
A system and a method for laser-driven propulsion, comprising transferring momentum to a projectile through a low-density material at laser fluences below plasma ablation threshold, the method comprising providing a metal layer having a ...  
WO/2018/093761A1
In an example embodiment, an attitude, orbit, and de-orbit control system (AODCS) for a satellite is provided. In an example embodiment, the AODCS system comprises one or more selectively retractable booms. The one or more selectively re...  
WO/2018/087541A1
A deployable wrapped rib assembly is disclosed, comprising a hub, a plurality of ribs each being connected to the hub at a fixed angle such that each rib is inclined with respect to a perimeter of the hub, each one of the plurality of ri...  
WO/2018/087273A1
The invention relates to a spacecraft (100) comprising a main body (110) and an attitude control system, said attitude control system including active attitude control means (150). In addition, the attitude control system also comprises ...  
WO/2018/078258A1
The attachment system (4) for a spacecraft (1) comprises a first support structure (5), a second support structure (6), and an attachment (7) in order to mechanically link the first structure (5) to the second structure (6). The second s...  
WO/2018/076780A1
A plate folding and unfolding device and a solar panel structure. The plate folding and unfolding device comprises: cams (120, 220, 320) fixed with first plates (111, 211) and provided therein with rotating shafts (130, 230, 330) in the ...  
WO/2018/075083A1
Systems, methods, and software described herein provide enhancements for deploying applications in satellites. In one example, a satellite may receive software applications capable of execution as virtual nodes on the satellite, and rece...  
WO/2018/071645A1
A microsatellite may include a module having a power source and a housing for containing an experiment, a drag device structurally configured to facilitate an orbit of the microsatellite when the microsatellite is deployed in space, wher...  
WO/2018/069994A1
The present invention suppresses, without greatly increasing the mass of a satellite, the time average peak value of a low-frequency magnetic noise or a low-frequency conduction noise generated from a power supply device which drives a h...  
WO/2018/071070A1
An impulse momentum propulsion apparatus includes a power source and a track arranged radially relative to a vertical axis with a proximal end of the track nearest the vertical axis and a distal end of the track farthest from the vertica...  

Matches 1 - 50 out of 13,538