ES2123154T3 - Acelerador de plasma con arrastre cerrado de electrones. - Google Patents

Acelerador de plasma con arrastre cerrado de electrones.

Info

Publication number
ES2123154T3
ES2123154T3 ES94927135T ES94927135T ES2123154T3 ES 2123154 T3 ES2123154 T3 ES 2123154T3 ES 94927135 T ES94927135 T ES 94927135T ES 94927135 T ES94927135 T ES 94927135T ES 2123154 T3 ES2123154 T3 ES 2123154T3
Authority
ES
Spain
Prior art keywords
magnetic
accelerator
trailer
side wall
plasma accelerator
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
ES94927135T
Other languages
English (en)
Inventor
Vladimir Vasilievich Gopanchuk
Igor Borisovich Sorokin
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Group SAS
Original Assignee
Airbus Group SAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Airbus Group SAS filed Critical Airbus Group SAS
Application granted granted Critical
Publication of ES2123154T3 publication Critical patent/ES2123154T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03H—PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03H1/00—Using plasma to produce a reactive propulsive thrust
    • F03H1/0037—Electrostatic ion thrusters
    • F03H1/0062—Electrostatic ion thrusters grid-less with an applied magnetic field
    • F03H1/0075—Electrostatic ion thrusters grid-less with an applied magnetic field with an annular channel; Hall-effect thrusters with closed electron drift
    • H—ELECTRICITY
    • H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05H—PLASMA TECHNIQUE; PRODUCTION OF ACCELERATED ELECTRICALLY-CHARGED PARTICLES OR OF NEUTRONS; PRODUCTION OR ACCELERATION OF NEUTRAL MOLECULAR OR ATOMIC BEAMS
    • H05H1/00—Generating plasma; Handling plasma
    • H05H1/54—Plasma accelerators

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Plasma & Fusion (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Spectroscopy & Molecular Physics (AREA)
  • Plasma Technology (AREA)
  • Particle Accelerators (AREA)
  • Crystals, And After-Treatments Of Crystals (AREA)
  • Electron Sources, Ion Sources (AREA)
  • Ignition Installations For Internal Combustion Engines (AREA)
  • Acyclic And Carbocyclic Compounds In Medicinal Compositions (AREA)

Abstract

EL ACELERADOR PROPUESTO COMPRENDE UN SISTEMA MAGNETICO (2), QUE TIENE UN POLO MAGNETICO EXTERNO (10) Y UN POLO MAGNETICO INTERNO (9) QUE ESTAN INTERCONECTADOS POR UN CIRCUITO MAGNETICO (8), UNA PANTALLA MAGNETICA EXTERIOR (13), UNA PANTALLA MAGNETICA INTERIOR (12), UNA BOBINA MAGNETIZANTE CENTRAL (5) Y BOBINAS DE MAGNETIZACION EXTERNA (7). ADEMAS, EL ACELERADOR TIENE UNA CAMARA DE DESCARGA (3) QUE COMPRENDE UN ANODO CONCAVO (18) RODEANDO LAS SUPERFICIES DE LAS FUERZAS MAGNETICAS (25) DE UNA ZONA DE IONIZACION (22), UN DISTRIBUIDOR DE GAS SECCIONAL (26), UNA PARED LATERAL INTERIOR (15) Y UNA PARED LATERAL EXTERIOR (16), LAS SUPERFICIES INTERNAS (20) DE ESA FORMA SON LOCALIZADAS EN LA ZONA DE IONIZACION (22) EN UN ANGULO PARA UN EJE LONGITUDINAL (A-A) DEL ACELERADOR.
ES94927135T 1994-08-25 1994-08-25 Acelerador de plasma con arrastre cerrado de electrones. Expired - Lifetime ES2123154T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/RU1994/000208 WO1996006518A1 (en) 1994-08-25 1994-08-25 Plasma accelerator with closed electron drift

Publications (1)

Publication Number Publication Date
ES2123154T3 true ES2123154T3 (es) 1999-01-01

Family

ID=20129882

Family Applications (1)

Application Number Title Priority Date Filing Date
ES94927135T Expired - Lifetime ES2123154T3 (es) 1994-08-25 1994-08-25 Acelerador de plasma con arrastre cerrado de electrones.

Country Status (9)

Country Link
US (1) US5798602A (es)
EP (1) EP0784417B1 (es)
JP (1) JPH11505058A (es)
AT (1) ATE173130T1 (es)
DE (1) DE69414421T2 (es)
DK (1) DK0784417T3 (es)
ES (1) ES2123154T3 (es)
UA (1) UA32449C2 (es)
WO (1) WO1996006518A1 (es)

Families Citing this family (35)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6612105B1 (en) 1998-06-05 2003-09-02 Aerojet-General Corporation Uniform gas distribution in ion accelerators with closed electron drift
US6215124B1 (en) 1998-06-05 2001-04-10 Primex Aerospace Company Multistage ion accelerators with closed electron drift
US6208080B1 (en) 1998-06-05 2001-03-27 Primex Aerospace Company Magnetic flux shaping in ion accelerators with closed electron drift
US6075321A (en) * 1998-06-30 2000-06-13 Busek, Co., Inc. Hall field plasma accelerator with an inner and outer anode
FR2782884B1 (fr) * 1998-08-25 2000-11-24 Snecma Propulseur a plasma a derive fermee d'electrons adapte a de fortes charges thermiques
US6150764A (en) * 1998-12-17 2000-11-21 Busek Co., Inc. Tandem hall field plasma accelerator
RU2162624C1 (ru) * 1999-05-26 2001-01-27 Байдаков Сергей Георгиевич Способ ускорения ионов и устройство для его реализации
DE19937033A1 (de) * 1999-08-05 2001-02-08 Volkswagen Ag Entlüftungsvorrichtung für ein Kurbelgehäuse einer Brennkraftmaschine
US6486593B1 (en) 2000-09-29 2002-11-26 The United States Of America As Represented By The United States Department Of Energy Plasma accelerator
RU2202049C2 (ru) * 2000-10-04 2003-04-10 Федеральное государственное унитарное предприятие Российского авиационно-космического агентства "Опытное конструкторское бюро "Факел" Плазменный двигатель с замкнутым дрейфом электронов
RU2196396C2 (ru) * 2000-10-23 2003-01-10 Петросов Валерий Александрович Способ регулирования вектора тяги электроракетного двигателя и устройство для его реализации
RU2196397C2 (ru) * 2000-12-28 2003-01-10 Петросов Валерий Александрович Способ и устройство для ускорения ионов в плазменных ускорителях холловского типа
RU2191292C2 (ru) * 2000-12-28 2002-10-20 Федеральное государственное унитарное предприятие Российского космического агентства "Опытное конструкторское бюро "Факел" Способ создания реактивной тяги в космосе
RU2187218C1 (ru) * 2001-05-16 2002-08-10 Алексеев Валерий Венедиктович Источник ионов (варианты)
DE10130464B4 (de) * 2001-06-23 2010-09-16 Thales Electron Devices Gmbh Plasmabeschleuniger-Anordnung
US6982520B1 (en) * 2001-09-10 2006-01-03 Aerojet-General Corporation Hall effect thruster with anode having magnetic field barrier
US6872929B2 (en) * 2003-04-17 2005-03-29 The Regents Of The University Of Michigan Low-noise, crossed-field devices such as a microwave magnetron, microwave oven utilizing same and method of converting a noisy magnetron to a low-noise magnetron
RU2244158C1 (ru) * 2003-05-23 2005-01-10 Федеральное государственное унитарное предприятие Российского космического агентства "Опытное конструкторское бюро "Факел" Способ прогнозирования параметров стационарного плазменного двигателя в процессе выработки ресурса
JP2006147449A (ja) 2004-11-24 2006-06-08 Japan Aerospace Exploration Agency 高周波放電プラズマ生成型二段式ホール効果プラズマ加速器
US7617092B2 (en) * 2004-12-01 2009-11-10 Microsoft Corporation Safe, secure resource editing for application localization
US7624566B1 (en) 2005-01-18 2009-12-01 The United States Of America As Represented By The Administrator Of National Aeronautics And Space Administration Magnetic circuit for hall effect plasma accelerator
US7500350B1 (en) 2005-01-28 2009-03-10 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Elimination of lifetime limiting mechanism of hall thrusters
RU2292678C1 (ru) * 2005-06-01 2007-01-27 Федеральное государственное унитарное предприятие Федерального космического агентства "Опытное конструкторское бюро "Факел" Способ создания ускоренного потока ионов
US7622721B2 (en) * 2007-02-09 2009-11-24 Michael Gutkin Focused anode layer ion source with converging and charge compensated beam (falcon)
RU2338294C1 (ru) * 2007-02-13 2008-11-10 Институт физики прочности и материаловедения Сибирского отделения Российской академии наук (ИФПМ СО РАН) Широкоапертурный источник газовых ионов
WO2008105736A2 (en) 2007-03-01 2008-09-04 Plasmatrix Materials Ab Method, material and apparatus for enhancing dynamic stiffness
CN102782320B (zh) * 2010-03-01 2015-01-28 三菱电机株式会社 霍尔推进器及宇宙航行体及推进方法
RU2458249C1 (ru) * 2011-03-31 2012-08-10 Государственный научный центр Российской Федерации - федеральное государственное унитарное предприятие "Исследовательский Центр имени М.В. Келдыша" Способ очистки рабочей части ускорительного канала стационарного плазменного двигателя от продуктов эрозии
FR2985292B1 (fr) * 2011-12-29 2014-01-24 Onera (Off Nat Aerospatiale) Propulseur plasmique et procede de generation d'une poussee propulsive plasmique
WO2015002131A1 (ja) * 2013-07-02 2015-01-08 学校法人日本大学 磁化同軸プラズマ生成装置
IL256341A (en) 2017-12-14 2018-01-31 Technion Res & Development Found Ltd The god engine has a narrow channel
US11530690B2 (en) 2019-02-13 2022-12-20 Technion Research & Development Foundation Ltd. Ignition process for narrow channel hall thruster
FR3094557B1 (fr) 2019-03-26 2024-03-01 2 Univ De Versailles Saint Quentin En Yvelines Dispositif d’éjection d’ions à effet Hall
RU2735043C1 (ru) * 2020-05-20 2020-10-27 Николай Борисович Болотин Плазменно-ионный ракетный двигатель
CN114776547B (zh) * 2022-03-28 2024-08-02 广州大学 一种无燃料卫星推进装置及推进方法

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0463408A3 (en) * 1990-06-22 1992-07-08 Hauzer Techno Coating Europe Bv Plasma accelerator with closed electron drift
EP0541309B1 (en) * 1991-11-04 1996-01-17 Fakel Enterprise Plasma accelerator with closed electron drift
US5359258A (en) * 1991-11-04 1994-10-25 Fakel Enterprise Plasma accelerator with closed electron drift
FR2693770B1 (fr) * 1992-07-15 1994-10-14 Europ Propulsion Moteur à plasma à dérive fermée d'électrons.
US5475354A (en) * 1993-06-21 1995-12-12 Societe Europeenne De Propulsion Plasma accelerator of short length with closed electron drift

Also Published As

Publication number Publication date
EP0784417B1 (en) 1998-11-04
US5798602A (en) 1998-08-25
EP0784417A1 (en) 1997-07-16
WO1996006518A1 (en) 1996-02-29
DK0784417T3 (da) 1999-07-19
DE69414421T2 (de) 1999-06-24
DE69414421D1 (de) 1998-12-10
JPH11505058A (ja) 1999-05-11
ATE173130T1 (de) 1998-11-15
UA32449C2 (uk) 2000-12-15
EP0784417A4 (en) 1997-06-04

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