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9 results about "Outer space" patented technology

Outer space, or simply space, is the expanse that exists beyond the Earth and between celestial bodies. Outer space is not completely empty—it is a hard vacuum containing a low density of particles, predominantly a plasma of hydrogen and helium, as well as electromagnetic radiation, magnetic fields, neutrinos, dust, and cosmic rays. The baseline temperature of outer space, as set by the background radiation from the Big Bang, is 2.7 kelvins (−270.45 °C; −454.81 °F). The plasma between galaxies accounts for about half of the baryonic (ordinary) matter in the universe; it has a number density of less than one hydrogen atom per cubic metre and a temperature of millions of kelvins; local concentrations of this plasma have condensed into stars and galaxies. Studies indicate that 90% of the mass in most galaxies is in an unknown form, called dark matter, which interacts with other matter through gravitational but not electromagnetic forces. Observations suggest that the majority of the mass-energy in the observable universe is dark energy, a type of vacuum energy that is poorly understood. Intergalactic space takes up most of the volume of the universe, but even galaxies and star systems consist almost entirely of empty space.

Collision avoidance assistance device, space information recorder, and collision avoidance assistance method

An object is to more accurately assist avoidance of a collision between space objects such as satellites or space debris in outer space. A recorder processing unit (110) acquires flight forecast information (401) indicating a flight forecast of each of a plurality of space objects (60) from a management business device (40) used by a management business operator that manages the plurality of space objects (60). Based on the acquired flight forecast information (401), the recorder processing unit (110) sets a forecast epoch of an orbit of each of the plurality of space objects (60), a forecast orbital element that identifies the orbit, and a forecast error that is forecast for the orbit, as orbit forecast information (51). The recorder processing unit (110) stores a space information recorder (50) including the orbit forecast information (51) in a storage unit (140).
Owner:MITSUBISHI ELECTRIC CORP

System for in SITU resource utilization in extraterrestrial environments

Systems and methods for the in situ extraction of materials, for example lunar regolith, from a celestial body. The systems and methods described herein can be used in outer space or on Earth. A high pressure gas is delivered to loosen up the material and form a borehole. A deployable mast deploys from a stowed, coiled configuration to a linear, deployed configuration into the borehole. A deployable tube may deploy to assist with delivering the gas and / or collecting the loosened material. One or more jets emit the gas. The jets may be supported at a free end of the tube or mast. The jets may direct loosened material through the tube and / or mast toward a collection reservoir. A flow separator may filter the loosened material from the gasses.
Owner:HONEYBEE ROBOTICS LTD

Positioning method, lunar positioning system, and positioning satellite

A flying object flies in an outer space from the earth to the moon or a planet or near the moon or a planet. The flying object includes a positioning-signal reception device. A ground station includes a positioning-signal transmission device equipped with a directivity-direction control function and has known position coordinates in an earth-fixed coordinate system. The flying object measures position coordinates in the earth-fixed coordinate system by receiving a positioning signal transmitted from the ground station simultaneously from the ground stations at four locations.
Owner:MITSUBISHI ELECTRIC CORP

Future note (documentation archive) + dark matter detection method (optical lattice clock)

InactiveJP2026027565AMeasurement devicesOptical latticeDark matter
In the current space navigation, communication, and defense technologies, it is difficult to integrate local control of time, gravity operation, use of dark matters, and communication with the outer space (the Buddhist monk Tenkai's gyrus), and intergalaxy communication, ultrahigh-speed movement, and creation of a time acceleration / deceleration space cannot be realized by modern technologies.SOLUTION: The present invention is a future note related to an ultra-future space technology capable of integrally operating time, gravity, and material behavior by performing local and large-scale dark matter control by a BHc / WHc gate based on a dark matter fluid space model and a space gate theory.SELECTED DRAWING: None
Owner:田中 芳明

System for in SITU resource utilization in extraterrestrial environments

Systems and methods for the in situ extraction of materials, for example lunar regolith, from a celestial body. The systems and methods described herein can be used in outer space or on Earth. A high pressure gas is delivered to loosen up the material and form a borehole. A deployable mast deploys from a stowed, coiled configuration to a linear, deployed configuration into the borehole. A deployable tube may deploy to assist with delivering the gas and / or collecting the loosened material. One or more jets emit the gas. The jets may be supported at a free end of the tube or mast. The jets may direct loosened material through the tube and / or mast toward a collection reservoir. A flow separator may filter the loosened material from the gasses.
Owner:HONEYBEE ROBOTICS LTD

Positioning method, lunar positioning system, and positioning satellite

A flying object flies in an outer space from the earth to the moon or a planet or near the moon or a planet. The flying object includes a positioning-signal reception device. A ground station includes a positioning-signal transmission device equipped with a directivity-direction control function and has known position coordinates in an earth-fixed coordinate system. The flying object measures position coordinates in the earth-fixed coordinate system by receiving a positioning signal transmitted from the ground station simultaneously from the ground stations at four locations.
Owner:MITSUBISHI ELECTRIC CORP

Positioning satellite

A flying object flies in an outer space from the earth to the moon or a planet or near the moon or a planet. The flying object includes a positioning-signal reception device. A ground station includes a positioning-signal transmission device equipped with a directivity-direction control function and has known position coordinates in an earth-fixed coordinate system. The flying object measures position coordinates in the earth-fixed coordinate system by receiving a positioning signal transmitted from the ground station simultaneously from the ground stations at four locations.
Owner:MITSUBISHI ELECTRIC CORP

A device and method for measuring well depth based on radiation cooling principle

The present invention belongs to the field of optical devices. In order to solve the problem that the well depth cannot be measured by passive power supply at night, a device and method for measuring the well depth based on the radiation cooling principle are disclosed. The device and method include an anti-flow air layer, an emission layer of radiation cooling material, and a reflection layer with high reflectivity of sunlight in the direction of the sky. The anti-flow air layer is used to prevent moisture and flowing air in the well from affecting the measurement results of the device. The emission layer of the radiation cooling material is used to radiate heat to the outer space through a transparent window of 8 to 13 microns in the atmosphere. The reflection layer with high reflectivity of sunlight is used to reflect more than 90% of sunlight in the 0.3 to 25 micron band, thereby reducing heat absorption. The technical solution can use a radiation cooling device to achieve well depth measurement.
Owner:SUZHOU UNIV

Method and apparatus for plasma model analysis of space charge effects

This application discloses a plasma model analysis method and apparatus for space charging and discharging effects. The method includes: determining the orbit type and the space region traversed during on-orbit operation; determining the plasma model of the outer space plasma fusion model in the traversed space region; obtaining plasma parameters of the traversed space region based on data from the current solar activity period and / or the current geomagnetic activity period; analyzing the charging and discharging effects occurring on the spacecraft surface based on the plasma parameters; using an intrinsic plasma model in the intrinsic region and a transitional fusion model in the transition region, determining the range of the transition region based on the boundary between two adjacent intrinsic regions; dividing the transition region into multiple sub-regions based on the range and division strategy of the transition region; determining the fusion mode of each sub-region for each sub-region, obtaining a transitional fusion model corresponding to the transition region. The plasma parameters obtained through plasma model analysis are more accurate.
Owner:BEIJING NORMAL UNIVERSITY