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Matches 401 - 450 out of 1,303

Document Document Title
JP2019032156A
To provide a launch system, a launch vehicle and a method of launching a payload for delivery of the payload at a terrestrial location, an Earth orbital location, or an extraorbital location.A launch vehicle 200 of the present invention ...  
JP6472320B2  
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...  
JP6467659B2  
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...  
JP6461999B2  
JP6453774B2  
JP6448460B2  
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...  
JP6417389B2  
JP6412593B2  
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...  
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...  
JP6402020B2  
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...  
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 ...  
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...  
JP6389720B2  
JP6388491B2  
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...  
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...  
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 ...  
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...  
JP6360903B2  
JP6351958B2  
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...  
JP6318447B2  
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...  
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...  
JP6299792B2  
JP6297581B2  
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...  
JP6253664B2  
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 ...  
JP6218892B2  
JP6214874B2  
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...  
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 ...  
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 ...  
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...  
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...  
JP2015214956A5  
JP2015222705A5  
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...  
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...  
JP2015222069A5  
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...  
JP6120878B2  
JP2016516172A5  
JP6096763B2  

Matches 401 - 450 out of 1,303