Login| Sign Up| Help| Contact|

Patent Searching and Data


Matches 301 - 350 out of 12,084

Document Document Title
WO/2022/176889A1
A monitoring system (404) has a plurality of monitoring satellites each equipped with a monitoring device and a communication device. A satellite information transmission system (403) has a plurality of communication satellites each equi...  
WO/2022/176893A1
Provided is a method for using a monitoring system and a communication system to detect the launch of a flying object and transmit flying object information to a handling system in quasi-real-time. A plurality of satellite constellatio...  
WO/2022/176894A1
Provided is a flight path prediction method for highly accurately predicting the flight path of a glide vehicle. A model database (350) stores a plurality of flight path models. A ground system (340) references the model database (350) w...  
WO/2022/176895A1
The purpose of the present invention is to provide a communication route searching method for quickly and accurately searching for a communication route for transmitting projectile information detected by a surveillance satellite. In a c...  
WO/2022/171588A1
The invention describes a boom system (100) for a satellite, comprising a boom (2) which is wound up in several layers in a wound-up state and is unwound in an unwound state, wherein the boom (2) is designed to assume a predetermined sha...  
WO/2022/109747A9
A satellite with deployable optics is provided. The satellite has a frame, an optical axis, and a deployable optical system. The optical system has a mechanical aperture perpendicular to the optical axis, where light collected travels su...  
WO/2022/167539A1
The invention relates to a launch vehicle comprising a rocket body (2; 102) that has a longitudinal axis (Z, Z'), which rocket body has at least one propulsion stage (3; 103) that can be propelled by a jet propulsion means (36; 136) that...  
WO/2022/168319A1
An extension boom (120) is extended from a state in which the extension boom (120) is wound into a tubular shape in an extension direction coinciding with one side in the widthwise direction of the tubular shape. Protruding portions (125...  
WO/2022/163804A1
Provided is a mirror support mechanism capable of alleviating deformation caused by compressive force or tensile force occurring in a support member. This mirror support mechanism supports a reflection mirror 1 which has a supported pa...  
WO/2022/155717A1
The present invention relates to a novel form of air, land, subsea or space propulsion, achieved through the use of appropriate electromagnetic interactions. By using capacitors formed by symmetrical or asymmetrical conductors (1) and (2...  
WO/2022/159166A1
Polymeric electro spray emitters and related methods are generally described. In some embodiments, an emitter may be made from an ionic electro active polymer. The composition of the electro spray emitters described herein may enable the...  
WO/2022/153639A1
According to an aspect of the present invention, there is provided a method comprising: propelling a servicing spacecraft to an object; deploying one or more counter mass(es) away from a servicing spacecraft bus to offset the center of m...  
WO/2022/153619A1
According to an aspect of the present invention, there is provided a method for rendezvous with an orbiting object comprising: launching a tug and a servicer into a client orbit; separating the servicer from the tug; and docking the serv...  
WO/2022/150370A1
A method of in-space assembly includes: providing a roll of spooled high strength composite (HSC) boom, a robotic arm, and a printhead disposed at about an end of the robotic arm, the roll of spooled high strength composite boom feedingl...  
WO/2021/236585A9
An apparatus, system and method are provided for launching, deploying and moving mobility platforms used to produce a three-dimensional product using additive printing. The product, or object, is made by collecting materials in-situ at a...  
WO/2022/150492A1
A method of generating a momentum change in a vehicle by phase changing matter in a closed system is used to change the momentum of the vehicle without the need of a combustion system for propulsion. The method uses the multi-phase dynam...  
WO/2022/147507A1
A device and method for emitting an electrospray of ionized particles is disclosed, comprising a reservoir, an emitter in communication with the reservoir and having openings, wherein the openings are configured to permit release of the ...  
WO/2022/145303A1
The present invention addresses the problem of improving space efficiency in placement in an aircraft. A front-side battery pack 30 is installed in a spacecraft 1 having a curved outer wall 11. The front-side battery pack 30 comprises a ...  
WO/2022/146279A1
The present invention relates to a table (2) on which additive manufacturing is carried out; a plurality of panels (3) which are produced by the additive manufacturing method and surround a plurality of satellite elements (E) such as pay...  
WO/2022/144699A1
A method for the manufacture of a structural component (1) in composite material reinforced with stiffening stringers (2), defining, in use, at least part of an outer shell (3) of a vector (4) and comprising a skin (5) and a plurality of...  
WO/2022/137623A1
In the present invention, a first satellite (301) comprises: a first communication device (501) that communicates with a satellite flying ahead or behind in the same orbital plane; a second communication device (502) that communicates wi...  
WO/2022/137622A1
In a communication satellite system (10), each communication satellite (20) flying in a plane of an orbit such as an orbit (A), an orbit (B), or an orbit (C) includes an anteroposterior communication device for communicating with other c...  
WO/2022/137362A1
[Problem] To provide a spacecraft control system, a spacecraft control method, and a server device whereby it is possible to quickly transmit control data to a spacecraft. [Solution] In this invention, a spacecraft system includes: a plu...  
WO/2022/137411A1
In the present invention, a ground system (1) comprises: a reflection efficiency calculation unit (142) that calculates reflection efficiency of a mobile unit (2); a condition determination unit (143) that predicts the amount of light re...  
WO/2022/137344A1
This communication satellite system (10) is provided with a before-and-after communication device for each of communication satellites (20) flying on respective orbital planes of an orbit (A), an orbit (B), an orbit (C), etc., to communi...  
WO/2022/137341A1
This satellite constellation (110) comprises a plurality of artificial satellites that respectively fly in inclined circular orbits on six or more orbit surfaces that have a common orbit inclination angle and have north-south axes shifte...  
WO/2022/138053A1
This power control device is for a linear actuator 10 in a docking device 1 having a six-axis parallel link mechanism 5. A motor driver 11 for controlling the rotational speed of a motor M of the linear actuator 10 on the basis of a load...  
WO/2022/138182A1
The present technology relates to an artificial satellite and a ground system that make it possible to efficiently retain data within the artificial satellite. The artificial satellite comprises: an image processing unit that executes a ...  
WO/2022/138180A1
This technology pertains to a sensor device which enables sensor data to be efficiently stored and a data processing method therefor. The sensor device comprises: a control unit that generates feature amount data by executing a feature a...  
WO/2022/139942A1
Bi-modal propulsion systems and related methods are generally described. In some embodiments, a bi-modal propulsion system may employ a single propellant for both chemical thruster(s), operating at elevated pressures, and electrical thru...  
WO/2022/130407A1
The present invention relates to a combined launch vehicle and satellite system. More specifically relates to the satellite combined with the launch vehicle's upper stage to provide a more efficient system that includes tank separation t...  
WO/2022/132669A1
Systems, methods and device for payload transportation and high altitude atmospheric payload deployment. A gondola includes a frame which is configured to carry a payload, such as a rocket. The gondola includes a control system using a p...  
WO/2022/127313A1
The present invention discloses a high-precision angular velocity control method under short-time large-boundary interference. Orbital control information is brought into a posture control system by performing deep coupling analysis with...  
WO/2022/132335A1
A solar array may include a first rigid composite solar panel including solar cells secured to a first substrate. The solar array may further include a second rigid composite solar panel including solar cells secured to a second substrat...  
WO/2022/123244A1
The present invention relates to a system for power delivery to satellites. More particularly, the present invention relates to a method and system for providing power to orbiting satellites from ground stations on Earth using laser ligh...  
WO/2022/116955A1
A method for processing a double-layer structure of a spacecraft thrust chamber comprises: providing a first wall structure (1), a second wall structure (2) and ribs (4); bringing the first wall structure (1) and the second wall structur...  
WO/2022/118208A1
A spacecraft is equipped with a low and high thrust space propulsion system including at least one water reservoir (1) containing liquid water, a high thrust propulsion part and a low thrust propulsion part. The high thrust propulsion pa...  
WO/2022/115001A1
The group of inventions relates to the field of communicating visual information from outer space, preferably using a constellation of micro-class artificial Earth satellites. An artificial Earth satellite comprises a propulsion unit, an...  
WO/2022/115614A1
A composite material comprising a first shielding layer (210); at least one metal containing layer (208) over the first shielding layer; and a second shielding layer (206) over said at least one metal containing layer opposite of the fir...  
WO/2022/111227A1
A method and a system for assessing attitude stability using light sensing of an on-orbit star, comprising: step S1: after a satellite captures a star, adopting an inertial orientation attitude control mode; step S2: a satellite-borne ca...  
WO/2022/112718A1
A space transportation system (1) intended to be mounted on a space launcher (100) comprising a re-ignitable propulsion device (2) and orientable flaps (3) located at a second end (12) and a control unit (4), each flap (3) comprising act...  
WO/2022/104408A1
A plasma reactor is provided together with a method for generating kinetic energy to propel a craft. The reactor includes an inlet for plasma; a reactor core having an interior chamber and an exterior chamber, the interior chamber being ...  
WO/2022/109575A1
Systems and methods described herein include collapsible and deployable truss structures defining reduced volumes for compact storage.  
WO/2019/140219A9
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/2022/109515A1
A constellation of many satellites provide communication between devices such as user terminals (UTs) and ground stations that are connected to other networks, such as the Internet. A constellation management system (CMS) facilitates man...  
WO/2022/101625A1
UAV (400, 500, 600) systems and methods for simulation of reduced- gravity environments are disclosed. A UAV (400, 500, 600) system has an ascent vehicle (104), comprising ascent thrust means, and an aerodynamic, free fall descent UAV (1...  
WO/2022/100532A1
Provided is a clamp for an aerospace testing machine, comprising a bottom plate (1) and a mounting plate (2) welded to an outer wall on one side of the bottom plate (1); a servo motor (3) is connected to an outer wall at the top part of ...  
WO/2022/100531A1
An auxiliary propulsion device for an aerospace liquid propeller comprising a main propulsion device, a left auxiliary device (3), and a right auxiliary device (10). The main propulsion device comprises a housing (1). A thermal insulatio...  
WO/2022/102760A1
A communication control apparatus controls optical communication between a communication relay satellite and plural user satellites such that, when the communication relay satellite relays communication between the plural user satellites...  
WO/2022/103559A1
An electrical power system has a dual battery configuration that enables sufficient power supply for a spacecraft bus and a payload module being carried by the spacecraft. During a sunlight power mode, power is drawn from a solar array o...  

Matches 301 - 350 out of 12,084