ES2101870T3 - Motor de plasma con deriva cerrada de electrones. - Google Patents

Motor de plasma con deriva cerrada de electrones.

Info

Publication number
ES2101870T3
ES2101870T3 ES92919481T ES92919481T ES2101870T3 ES 2101870 T3 ES2101870 T3 ES 2101870T3 ES 92919481 T ES92919481 T ES 92919481T ES 92919481 T ES92919481 T ES 92919481T ES 2101870 T3 ES2101870 T3 ES 2101870T3
Authority
ES
Spain
Prior art keywords
channel
annular
anode
main
magnetic field
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
ES92919481T
Other languages
English (en)
Inventor
Alexei Morozov
Antonina Bougrova
Valentine Niskine
Alexei Dessijatskov
Dominique Valentian
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.)
Societe Europeenne de Propulsion SEP SA
Original Assignee
Societe Europeenne de Propulsion SEP SA
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 Societe Europeenne de Propulsion SEP SA filed Critical Societe Europeenne de Propulsion SEP SA
Application granted granted Critical
Publication of ES2101870T3 publication Critical patent/ES2101870T3/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)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Spectroscopy & Molecular Physics (AREA)
  • Plasma Technology (AREA)
  • Spark Plugs (AREA)

Abstract

EL MOTOR DE PLASMA COMPRENDE UN CANAL ANULAR PRINCIPAL DE IONIZACION Y DE ACELERACION (24) DELIMITADO POR PIEZAS (22) DE MATERIAL AISLANTE Y ABIERTO EN SU EXTREMO CORRIENTE ABAJO (225), AL MENOS UN CATODO HUECO (40) ASOCIADO A MEDIOS (41) DE ALIMENTACION DE GAS IONIZABLE, Y UN ANODO ANULAR (25) CONCENTRICO AL CANAL ANULAR PRINCIPAL (24) Y DISPUESTO A DISTANCIA DEL EXTREMO CORRIENTE ABAJO ABIERTO (225). UNA CAMARA TAMPON ANULAR (23) QUE PRESENTA EN EL SENTIDO RADIAL UNA DIMENSION MAYOR QUE LA DEL CANAL ANULAR PRINCIPAL (24) SE EXTIENDE CORRIENTE ARRIBA DE ESTE MAS ALLA DE LA ZONA EN LA QUE ESTA COLOCADO EL ANODO ANULAR (25). UNOS MEDIOS (26) DE ALIMENTACION DE GAS IONIZABLE DESEMBOCAN CORRIENTE ARRIBA DEL ANODO (259 A TRAVES DE UN DISTRIBUIDOR ANULAR (27) EN UNA ZONA DISTINTA DE LA ZONA QUE LLEVA EL ANODO (25). UNOS MEDIOS (31 33, 34 A 38) DE CREACION DE UN CAMPO MAGNETICO EN EL CANAL PRINCIPAL (24) SE ADAPTAN PARA PRODUCIR EN ESTE CANAL PRINCIPAL (24) UN CAMPO MAGNETICO ESENCIALMENTE RADIALQUE PRESENTA UN GRADIENTE CON UNA INDUCCION MAXIMA EN EL EXTREMO CORRIENTE ABAJO (225) DEL CANAL (24).
ES92919481T 1992-07-15 1992-09-01 Motor de plasma con deriva cerrada de electrones. Expired - Lifetime ES2101870T3 (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9208744A FR2693770B1 (fr) 1992-07-15 1992-07-15 Moteur à plasma à dérive fermée d'électrons.
CA002142607A CA2142607A1 (en) 1992-07-15 1993-06-21 A plasma accelerator of short length with closed electron drift

Publications (1)

Publication Number Publication Date
ES2101870T3 true ES2101870T3 (es) 1997-07-16

Family

ID=25677792

Family Applications (1)

Application Number Title Priority Date Filing Date
ES92919481T Expired - Lifetime ES2101870T3 (es) 1992-07-15 1992-09-01 Motor de plasma con deriva cerrada de electrones.

Country Status (9)

Country Link
US (1) US5581155A (es)
EP (1) EP0650557B1 (es)
JP (1) JP3083561B2 (es)
CA (1) CA2142607A1 (es)
DE (1) DE69219625T2 (es)
ES (1) ES2101870T3 (es)
FR (1) FR2693770B1 (es)
RU (1) RU2121075C1 (es)
WO (2) WO1994002738A1 (es)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2012035181A1 (es) * 2010-09-17 2012-03-22 Asociación De La Industria Navarra (Ain) Dispositivo de ionización

Families Citing this family (67)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0784417B1 (en) * 1994-08-25 1998-11-04 AEROSPATIALE Société Nationale Industrielle Plasma accelerator with closed electron drift
RU2092983C1 (ru) * 1996-04-01 1997-10-10 Исследовательский центр им.М.В.Келдыша Плазменный ускоритель
RU2088802C1 (ru) * 1995-12-09 1997-08-27 Исследовательский центр им.М.В.Келдыша Холловский двигатель
DE69637292T2 (de) * 1995-12-09 2008-11-06 Astrium Sas Steuerbarer Hall-Effekt-Antrieb
FR2743191B1 (fr) * 1995-12-29 1998-03-27 Europ Propulsion Source d'ions a derive fermee d'electrons
US5892329A (en) * 1997-05-23 1999-04-06 International Space Technology, Inc. Plasma accelerator with closed electron drift and conductive inserts
US6612105B1 (en) 1998-06-05 2003-09-02 Aerojet-General Corporation Uniform gas distribution in 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
US6215124B1 (en) 1998-06-05 2001-04-10 Primex Aerospace Company Multistage ion accelerators with closed electron drift
WO1999063222A1 (en) * 1998-06-05 1999-12-09 Primex Aerospace Company Uniform gas distribution in ion accelerators with closed electron drift
US6031334A (en) * 1998-06-17 2000-02-29 Primex Technologies, Inc. Method and apparatus for selectively distributing power in a thruster system
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
US6064156A (en) * 1998-09-14 2000-05-16 The United States Of America As Represented By The Administrator Of Nasa Process for ignition of gaseous electrical discharge between electrodes of a hollow cathode assembly
US6150764A (en) * 1998-12-17 2000-11-21 Busek Co., Inc. Tandem hall field plasma accelerator
RU2156555C1 (ru) * 1999-05-18 2000-09-20 Государственное унитарное предприятие "Всероссийский электротехнический институт им. В.И. Ленина" Способ получения и ускорения плазмы и ускоритель плазмы с замкнутым дрейфом электронов для его осуществления
US6334302B1 (en) 1999-06-28 2002-01-01 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Variable specific impulse magnetoplasma rocket engine
DE10014034C2 (de) * 2000-03-22 2002-01-24 Thomson Tubes Electroniques Gm Plasma-Beschleuniger-Anordnung
DE10014033C2 (de) * 2000-03-22 2002-01-24 Thomson Tubes Electroniques Gm Plasma-Beschleuniger-Anordnung
US6486593B1 (en) 2000-09-29 2002-11-26 The United States Of America As Represented By The United States Department Of Energy Plasma accelerator
WO2002104085A2 (en) * 2001-06-19 2002-12-27 Toky0 Electron Limited A closed-drift hall effect plasma vacuum pump for process reactors
DE10147998A1 (de) * 2001-09-28 2003-04-10 Unaxis Balzers Ag Verfahren und Vorrichtung zur Erzeugung eines Plasmas
DE10153723A1 (de) * 2001-10-31 2003-05-15 Thales Electron Devices Gmbh Plasmabeschleuniger-Anordnung
US6696792B1 (en) 2002-08-08 2004-02-24 The United States Of America As Represented By The United States National Aeronautics And Space Administration Compact plasma accelerator
US7461502B2 (en) 2003-03-20 2008-12-09 Elwing Llc Spacecraft thruster
FR2857555B1 (fr) 2003-07-09 2005-10-14 Snecma Moteurs Accelerateur a plasma a derive fermee d'electrons
DE602004024993D1 (de) * 2004-09-22 2010-02-25 Elwing Llc Antriebssystem für Raumfahrzeuge
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
US7420182B2 (en) * 2005-04-27 2008-09-02 Busek Company Combined radio frequency and hall effect ion source and plasma accelerator system
JP4816004B2 (ja) * 2005-10-28 2011-11-16 三菱電機株式会社 ホールスラスタ及び宇宙航行体
JP4816179B2 (ja) * 2006-03-20 2011-11-16 三菱電機株式会社 ホールスラスタ
WO2008056369A1 (en) * 2006-11-09 2008-05-15 Technion - Research & Development Foundation Ltd Low-power hall thruster
JP2008223655A (ja) * 2007-03-14 2008-09-25 Japan Aerospace Exploration Agency ホール型電気推進機
DE102007044074B4 (de) * 2007-09-14 2011-05-26 Thales Electron Devices Gmbh Elektrostatische Ionenbeschleunigeranordnung
US8407979B1 (en) 2007-10-29 2013-04-02 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Magnetically-conformed, variable area discharge chamber for hall thruster, and method
WO2010017185A1 (en) 2008-08-04 2010-02-11 Agc Flat Glass North America, Inc. Plasma source and methods for depositing thin film coatings using plasma enhanced chemical vapor deposition
FR2941503B1 (fr) * 2009-01-27 2011-03-04 Snecma Propulseur a derive fermee d'electrons
FR2950114B1 (fr) * 2009-09-17 2012-07-06 Snecma Moteur a effet hall avec refroidissement de la ceramique interne
FR2950115B1 (fr) * 2009-09-17 2012-11-16 Snecma Propulseur plasmique a effet hall
US8468794B1 (en) 2010-01-15 2013-06-25 The United States Of America As Represented By The Administrator Of National Aeronautics And Space Administration Electric propulsion apparatus
FR2959534B1 (fr) * 2010-04-29 2012-07-13 Snecma Moteur a effet hall avec regulation de la temperature du dispositif de chauffage de la cathode
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
FR2976029B1 (fr) 2011-05-30 2016-03-11 Snecma Propulseur a effet hall
US9679869B2 (en) 2011-09-02 2017-06-13 Skyworks Solutions, Inc. Transmission line for high performance radio frequency applications
FR2979956B1 (fr) 2011-09-09 2013-09-27 Snecma Systeme de propulsion electrique a propulseurs a plasma stationnaire
FR2986577B1 (fr) * 2012-02-06 2016-05-20 Snecma Propulseur a effet hall
US9054065B2 (en) * 2012-04-30 2015-06-09 Skyworks Solutions, Inc. Bipolar transistor having collector with grading
WO2013188712A1 (en) 2012-06-14 2013-12-19 Skyworks Solutions, Inc. Power amplifier modules including related systems, devices, and methods
RU2543103C2 (ru) * 2013-06-24 2015-02-27 Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" Ионный двигатель
US10273944B1 (en) * 2013-11-08 2019-04-30 The United States Of America As Represented By The Administrator Of National Aeronautics And Space Administration Propellant distributor for a thruster
CN103953517B (zh) * 2014-05-13 2016-08-31 哈尔滨工业大学 霍尔推进器改进装置
BR112017011612A2 (pt) 2014-12-05 2018-01-16 Agc Glass Europe, S.A fonte de plasma de cátodo oco
EP3228161B1 (en) 2014-12-05 2021-11-03 AGC Flat Glass North America, Inc. Plasma source utilizing a macro-particle reduction coating and method of using a plasma source utilizing a macro-particle reduction coating for deposition of thin film coatings and modification of surfaces
US9721765B2 (en) 2015-11-16 2017-08-01 Agc Flat Glass North America, Inc. Plasma device driven by multiple-phase alternating or pulsed electrical current
US9721764B2 (en) 2015-11-16 2017-08-01 Agc Flat Glass North America, Inc. Method of producing plasma by multiple-phase alternating or pulsed electrical current
US10573499B2 (en) 2015-12-18 2020-02-25 Agc Flat Glass North America, Inc. Method of extracting and accelerating ions
US10242846B2 (en) 2015-12-18 2019-03-26 Agc Flat Glass North America, Inc. Hollow cathode ion source
JP2019501496A (ja) * 2015-12-18 2019-01-17 エージーシー フラット グラス ノース アメリカ，インコーポレイテッドＡｇｃ Ｆｌａｔ Ｇｌａｓｓ Ｎｏｒｔｈ Ａｍｅｒｉｃａ，Ｉｎｃ． イオンを抽出し、加速させるホロカソードイオン源および方法
RU2691702C2 (ru) * 2017-08-15 2019-06-17 Федеральное государственное бюджетное образовательное учреждение высшего образования Балтийский государственный технический университет "ВОЕНМЕХ" им. Д.Ф. Устинова (БГТУ "ВОЕНМЕХ") Гиперзвуковой прямоточный воздушно-реактивный двигатель
FR3094557B1 (fr) * 2019-03-26 2024-03-01 2 Univ De Versailles Saint Quentin En Yvelines Dispositif d’éjection d’ions à effet Hall
RU2726152C1 (ru) * 2019-12-09 2020-07-09 Федеральное государственное бюджетное военное образовательное учреждение высшего образования "Военно-космическая академия имени А.Ф. Можайского" Министерства обороны Российской Федерации Электрический ракетный двигатель (варианты)
US20230003202A1 (en) * 2021-04-15 2023-01-05 California Institute Of Technology Thermally managed electric propulsion systems
RU2764496C1 (ru) * 2021-04-20 2022-01-17 Публичное акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" Магнитоплазменный электрореактивный двигатель
CN115681057B (zh) * 2023-01-03 2023-06-02 国科大杭州高等研究院 一种霍尔推进系统及其运行方法

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4841197A (en) * 1986-05-28 1989-06-20 Nihon Shinku Gijutsu Kabushiki Kaisha Double-chamber ion source
US4862032A (en) * 1986-10-20 1989-08-29 Kaufman Harold R End-Hall ion source
JPS6477764A (en) * 1987-09-18 1989-03-23 Toshiba Corp Hall type ion thruster
EP0463408A3 (en) * 1990-06-22 1992-07-08 Hauzer Techno Coating Europe Bv Plasma accelerator with closed electron drift
DE69304336T2 (de) * 1993-06-21 1997-01-23 Europ De Propulsion S E P Soc Plasmamotor geringer länge mit geschlossenem elektronendrift

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2012035181A1 (es) * 2010-09-17 2012-03-22 Asociación De La Industria Navarra (Ain) Dispositivo de ionización

Also Published As

Publication number Publication date
JPH08500930A (ja) 1996-01-30
CA2142607A1 (en) 1995-01-05
WO1994002739A1 (fr) 1994-02-03
FR2693770A1 (fr) 1994-01-21
FR2693770B1 (fr) 1994-10-14
EP0650557B1 (fr) 1997-05-07
DE69219625T2 (de) 1997-11-13
EP0650557A1 (fr) 1995-05-03
WO1994002738A1 (fr) 1994-02-03
RU95105253A (ru) 1996-10-27
DE69219625D1 (de) 1997-06-12
RU2121075C1 (ru) 1998-10-27
JP3083561B2 (ja) 2000-09-04
US5581155A (en) 1996-12-03

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