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JP6472320B2 |
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JPWO2018061230A1 |
A cable (130) has an electric wire belt (134). A parallel electric wire (133) is put in order and constituted, without twisting the 1st electric wire (131) and 2nd electric wire (132) that accomplish one pair. A plurality of parallel ele...
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JP6467659B2 |
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JP2019502852A |
A thruster for micro satellites is indicated. A thruster includes a cathode which consists of promotion agent material, and an anode which consists of Ablative material. A thruster includes a housing which has a proximal end and a distal...
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JP6461999B2 |
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JP6453774B2 |
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JP6448460B2 |
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JP2018535353A |
The present invention relates to a microwave electric heat thruster (MET) suitable for space electric heat promotion, It has a variable frequency microwave electric heat thruster propulsion module which makes possible initial promotion o...
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JP6417389B2 |
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JP6412593B2 |
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JP2018163873A |
To provide a Z-pinch device which converts a liquid jet into a plasma while generating a conductive path.An infusion system 150 includes: a reservoir 152 housing liquid; a gate plate 216 having a cylindrical array of a gate plate opening...
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JP2018530475A |
A propulsion system contains an electric thruster of at least 1 group spatially arranged within a multiaxial system. A control device is communicating with each electric thruster. To impelling force of a circumference of two axes of a mu...
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JP6402020B2 |
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JP2018528358A |
A propulsion system is indicated on these specifications and it is a solid conductor or a semiconductor cathode (130), An anode (110) in which it is an anode (110) which has the potential difference to the cathode (130), and the potentia...
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JP2018527246A |
A system and a method for equipping with a thruster on a vehicle are explained by this specification. A thruster attached to the 1st, the 2nd, the 3rd rotation joint, a boom, a thruster palette, and a thruster palette can be included by ...
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JP2018526570A |
A reservoir (20) containing a conductive jacket (21) in which the present invention was provided with a chamber (10) and solid propellant (PS), was stored in a chamber (10), and possesses an orifice (22), It is a means (30, 40) to form i...
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JP6389720B2 |
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JP6388491B2 |
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JP2018525557A |
The Hall effect screw (10) constituted so that it might be arranged on the inner side or the outside of a spacecraft. A screw has a concentrator (36) for collecting particles (P). The shape of a concentrator is demarcated by the continua...
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JP2018127917A |
To provide a hall thruster capable of supplying propellant powder to a channel evenly without using a large-sized manifold, and greatly reducing a temperature of the propellant powder to be supplied to the channel.A channel 12 has, on it...
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JPWO2018003005A1 |
A reaction wheel (110) detects angular momentum. Satellite control machinery (120) chooses an object thruster based on detected angular momentum. An electric power unit (130) changes adjustment electric power to an object thruster. Flow ...
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JP2018116803A |
To provide an electric heater capable of improving heating efficiency and reliability while restraining up-sizing.An electric heater 40 includes a first electric heating member 41 generating heat by electrification, a second electric hea...
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JP6360903B2 |
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JP6351958B2 |
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JP2018090035A |
To put vertical take-off/landing machines and the like which are good in propulsion efficiency into practical use, eliminating the need for a specially high-performance (high-cost) engine and the like.Very plainly speaking, vertical take...
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JP6318447B2 |
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JP2018058393A |
To use materials being not present in an existing method (not conceivable) as propellant, and furthermore use it in an overlapping manner without running out of it, and thereby achieve space propulsion (pressure difference propulsion) sy...
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JP2018048555A |
This invention relates to a spaceship which travels by injecting a jet. It is necessary to sufficiently secure a cross section (contact cross section area) of a D(deuterium) particle flux. That is, an ion gas is created of D2O, or a plas...
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JP6299792B2 |
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JP6297581B2 |
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JP2018503774A |
The present invention relates to a spacecraft containing a Hall effect thruster and this thruster. Hall effect thruster 10 which is arranged to wall 22 inside and provided with magnetic circuit 30 and electric circuit 60 provided with ne...
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JP6253664B2 |
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JP2017537831A |
A system and a method of carrying out an electric power supply to the electric thruster (112) of a flight object (100). A method includes providing the electric propulsion system (104) of a flight object with the unadjusted high-voltage ...
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JP6218892B2 |
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JP6214874B2 |
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JP2017171144A |
To provide a device which can generate inverted thrust by a single unit, and can suppress weight to the minimum, in the air injection type thrust generation device for the posture control of a moving body.This device includes: a cylindri...
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JP2017522226A |
The present invention relates to the field, especially electric space promotion, of space promotion. The electrostatic thruster (101) in which the space propulsion system (100) of the present invention contains 1st at least one electric ...
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JP2017129115A |
To provide a structural propellant for ion rockets (SPIR).Systems, methods, and apparatus for a structural propellant for ion rockets (SPIR) are disclosed. A method for in-space propulsion of a spacecraft involves a step of removing, by ...
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JP2017520076A |
A set (31, 30, 40, 58) of a means for a device (100) to form ion * electron plasma in a chamber (20) and this chamber (20), It is a means (50) for making it accelerate besides a chamber which can extract electrification particles of plas...
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JP2017123310A |
To provide a plasma acceleration apparatus and a plasma acceleration method with good thrust efficiency.The plasma acceleration apparatus includes: a cathode 11 for supplying electrons to a plasma acceleration region; an anode 12; a powe...
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JP2015214956A5 |
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JP2015222705A5 |
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JP2017110665A |
To provide systems and methods for electromagnetic thrusting.An electromagnetic thrusting system includes an axially asymmetric resonant cavity 100 including a conductive inner surface, the axially asymmetric resonant cavity adapted to s...
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JP2017516021A |
A space flight object engine (10) provided with a chemicals thruster which has a nozzle (30) for emitting combustion gas with a Hall effect thruster. This engine is constituted so that a nozzle may function as a discharge channel for par...
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JP2015222069A5 |
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JP2017089655A |
To resolve some problems found in a posture control of the prior art spacecraft through permanent magnets that has been passive for stabilizing it and the spacecraft machine could not be faced to its optional direction, the prior art orb...
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JP6120878B2 |
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JP2016516172A5 |
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JP6096763B2 |
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JP6076984B2 |
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