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Matches 1 - 50 out of 14,470

Document Document Title
WO/2020/182692A3
The invention relates to an androgynous coupling means (10) exhibiting both male and female coupling sections, wherein the androgynous coupling means is configured for form fit coupling with at least one further androgynous coupling mean...  
WO/2021/001945A1
The present invention provides a spectroscopic imaging device (1) including: a spectroscopic unit (2) that includes a field diaphragm (2d), a shading optical element (2c), a dispersion element (2f), and a two dimensional detector (2h); a...  
WO/2021/000047A1
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/2020/242477A8
Propulsion systems, such as electro spray thrusters, may include an electrically actuated valve to permit a selective flow of propellant to a thruster. The valve may be located and arranged such that it physically separates a propellant,...  
WO/2020/261397A1
A device communication apparatus (950) communicates with at least one of a master satellite (310) and a slave satellite (320). A control unit (110) generates a control command (51) that controls the master satellite (310) and the slave s...  
WO/2020/261481A1
A satellite constellation (100) is provided with a plurality of artificial satellites (110). The plurality of artificial satellites each travel around an inclined circular orbit multiple times per day. Normal lines to a plurality of orbi...  
WO/2020/260662A1
Systems and methods for determining parameters suitable for determining an orbit of a satellite using TDOA parameters and several spaced receivers.  
WO/2020/256024A1
A satellite constellation formation system forms a satellite constellation (20) having an N number (N being a natural number) of orbital planes (21) having mutually different normal directions. A satellite constellation formation unit fo...  
WO/2020/255310A1
A satellite constellation formation system forms a satellite constellation (20) having an N number (N being a natural number) of orbital planes (21) having mutually different normal directions. A satellite constellation formation unit fo...  
WO/2020/256792A1
A structure for changing the attitude of a spacecraft is provided including an elongated member and a plurality of actuators coupled to the elongated member. The elongated member is coupled to the spacecraft. The elongated member has a l...  
WO/2020/257649A1
Various embodiments of a vortex thruster system is described herein that is configured to create at least three discrete thrust levels. In some embodiments, the vortex thruster system is configured to decompose a monopropellant and deliv...  
WO/2020/250131A2
The present invention relates to a tank for containing a component fluid or a mixture of components.  
WO/2020/250709A1
The present technology relates to an artificial satellite and a control method for the same that can reduce battery consumption and guarantee the quality of captured images. An artificial satellite is provided with an image capturing dev...  
WO/2020/250706A1
The present technology pertains to: an image processing method enabling image processing on a plurality of captured images obtained through operation of formation flight; and a metadata data structure. In the present technology, an image...  
WO/2020/250708A1
The present technology pertains to: an image management method enabling management of an image captured by an artificial satellite; and a metadata data structure. In the present technology, a management device for managing an image captu...  
WO/2020/249987A1
The subject of the present invention relates to a floating platform (10) for launching a space rocket (100) from high altitude comprising a support structure (20) for suspending the space rocket (100) and which support structure (20) can...  
WO/2020/249831A1
Multiple hold-down and release device (1) for spacecraft, that comprises: - a central structure (2) comprising: - a central section (3) with an inner hole (4) with a cylindrical surface comprising an end stop (5), an inner axial shaft (6...  
WO/2020/250707A1
The present invention pertains to: a satellite system imaging method which, in satellite remote sensing, enables an artificial satellite to capture an image in response to an event that has taken place on the ground; and a transmitting d...  
WO/2020/245897A1
A landing gear (100) comprises a leg (110A, 110B, 110C), a rotating body (130A, 130B, 130C), and a housing (150). The leg (110A, 110B, 110C) makes contact with the landing surface at one end and moves linearly in the axial direction with...  
WO/2020/245549A1
A space aircraft (1) comprises a fuselage (3), two wings (4A, 4B) arranged on either side of the fuselage (3), and two nacelles (7A, 7B) arranged at the ends of the wings (4A, 4B) and each carrying a horizontal tail (8A, 8B) and a vertic...  
WO/2020/246951A1
A reconfigurable power processing unit for a spacecraft including a plurality of power modules. Each of the power modules includes a first power source and a second power source. The first power source and the second power source are con...  
WO/2020/246168A1
This method for estimating a right-under point position of an on-orbit object comprises: a photographing step for photographing an observation image of the on-orbit object (X) together with a known object of which orbit is known; a first...  
WO/2020/245193A1
The invention relates to a method and a system for determining the capability of a sensor contained in a satellite to access a target region (8). The position (5) of the satellite is ascertained, the viewing radius of the sensor in the d...  
WO/2020/240826A1
A satellite constellation formation system in which each satellite in an orbit satellite group is provided with a propulsion device for changing the speed of each satellite in the orbit satellite group. A satellite constellation formatio...  
WO/2020/240824A1
This satellite constellation formation system forms a satellite constellation (20) including a plurality of orbital planes (21), each having a plurality of satellites flying at the same orbital height. A satellite constellation formation...  
WO/2020/242477A1
Propulsion systems, such as electro spray thrusters, may include an electrically actuated valve to permit a selective flow of propellant to a thruster. The valve may be located and arranged such that it physically separates a propellant,...  
WO/2020/240825A1
A satellite constellation formation system forms a satellite constellation (20) that includes two orbital planes which have differing normal-line orientations and in which the same number of satellites travel. A satellite constellation f...  
WO/2020/236961A1
An electrospray apparatus including a plurality of emitters, disposed on a substrate, wherein the plurality of emitters can have a narrow parameter distribution, and where the apparatus can optionally include one or more control systems,...  
WO/2020/236256A1
A space optical system is disclosed. The space optical system (100) includes a primary support structure (110) in support of a primary mirror (111). The space optical system also includes a sensor mounting structure (101) coupled to the ...  
WO/2020/234529A1
The present description relates to a device (7) for recognising the attitude of an object, characterized in that it comprises: a sphere (11) comprising a wall (13) able to let a light flux at least partially pass; a ball (17), moveably m...  
WO/2020/234540A1
Space launcher comprising a launcher body (1), an engine (2), a combustion chamber (4), a nozzle (5) having a main axis (Z-Z), the nozzle (5) being provided with a plate (6) extending radially, the plate (6) having an inner face and an o...  
WO/2020/234539A1
Space launcher comprising a launcher body (1), an engine (2), a nozzle (5) provided with a plate (6) extending radially around the nozzle (5) or a combustion chamber (4) and insulating an internal volume of the spacecraft from an externa...  
WO/2020/181117A8
To manage propellant in a spacecraft, the method of this disclosure includes storing propellant in a tank as a mixture of liquid and gas; transferring the propellant out of the tank; converting the mixture of liquid and gas propellant in...  
WO/2020/231520A1
Embodiments of the present disclosure generally relate to protective coatings on an aerospace component and methods for depositing the protective coatings. The protective coating can be anti-coking coatings to reduce or suppress coke for...  
WO/2020/232388A1
An array of antenna assemblies each generate solar power and utilize the generated solar power at that antenna assembly, which enables large amounts of power to be generated. An antenna assembly having a flat antenna layer forming a firs...  
WO/2020/232386A1
An antenna array has a plurality of square or rectangular antenna assemblies. Each assembly includes a first antenna assembly surface with a solar cell and a second antenna assembly with one or more antenna elements. The antenna assembli...  
WO/2020/232337A1
A wafer-scale satellite bus and a manner of making the same include using wafer reconstruction techniques to stack functional diced circuits onto each other and bond them. The disclosed techniques allow for a variety of functions in each...  
WO/2020/231468A1
An apparatus includes multiple layers (102, 302) of phase-stable material, where adjacent layers of the phase-stable material are separated by multiple spaces (104, 304). The apparatus also includes liquid phase change material (106, 306...  
WO/2020/139188A8
An ion thruster (1, 1a) and a method for providing trust is disclosed. The ion thruster (1, 1a) comprises a first electrode (3, 3a), magnetic field generating device (2, 2a) providing a magnetic trap zone (MT) at the first electrode, and...  
WO/2020/226988A1
A method is provided for realigning or relieving mechanical stress in a spacecraft frame. The process includes providing a spacecraft which includes at least two frame subsections connected by a mechanical connector. The mechanical conne...  
WO/2020/222250A1
The invention relates to a dynamic wing assembly system for the re-entry vehicles comprising four cup-type oval shaped wings (33, 34, 35, 36) attached to the body of the re-entry vehicle by a movable connecting means; four inertial senso...  
WO/2020/222836A1
A circuit for igniting and sustaining an electron discharge includes an ignitor circuit. The igniter circuit includes a high voltage transformer and a switch connected in series between a primary of the transformer and a DC source return...  
WO/2020/223733A1
Exemplary embodiments provided herein include an attachment and deployment system and method. Exemplary embodiments may use features together or separately as desired. The attachment feature may be used to periodically couple a solar sail.  
WO/2020/218569A1
A nose fairing (10) is coupled to a main body (12) of a rocket (11) so as to be capable of separating therefrom. This nose fairing comprises: a pair of fairing pieces (40), (50) which are capable of separating after a prescribed time has...  
WO/2020/217340A1
This satellite constellation (200) is provided with three artificial satellites (210A-210C) which monitor a target region on the earth (101). Each artificial satellite has an elliptical orbit that is heliosynchronous and has an orbital i...  
WO/2020/190349A3
Systems for insulating a space vehicle or space borne container from an external environment as well as cryogens from heat sources. Such systems also protect the vehicle from the high dynamic pressures, the high heat loads encountered in...  
WO/2020/214381A1
An apparatus includes a structure (100, 300, 700) configured to receive and transport thermal energy. The structure includes one or more materials configured to undergo a solid-solid phase transformation at a specified temperature or in ...  
WO/2020/209136A1
The objective of the present invention is to provide a toilet for microgravity space with which it is possible to limit electric power usage for recirculating air, using a simple configuration for a toilet bowl. A simple toilet device 10...  
WO/2020/205174A1
Networked initiation systems for hold-down and release mechanisms (HDRMs) are described. The systems include a control unit, a plurality of firing control units operably connected to and in communication with the control unit, wherein ea...  
WO/2020/206096A1
Systems, apparatuses, methods, and software are described herein that provide enhanced logistical control over spacecraft. This logistical control can include attitude adjustment and desaturation of reaction wheels. In one example, a met...  

Matches 1 - 50 out of 14,470