DE69914987D1 - Auf hohen thermischen Belastungen abgestimmter Plasmamotor mit geschlossenem Elektronendrift - Google Patents

Auf hohen thermischen Belastungen abgestimmter Plasmamotor mit geschlossenem Elektronendrift

Info

Publication number
DE69914987D1
DE69914987D1 DE69914987T DE69914987T DE69914987D1 DE 69914987 D1 DE69914987 D1 DE 69914987D1 DE 69914987 T DE69914987 T DE 69914987T DE 69914987 T DE69914987 T DE 69914987T DE 69914987 D1 DE69914987 D1 DE 69914987D1
Authority
DE
Germany
Prior art keywords
high thermal
thermal loads
electron drift
closed electron
plasma motor
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
DE69914987T
Other languages
English (en)
Other versions
DE69914987T2 (de
Inventor
Dominique Valentian
Jean-Pierre Bugeat
Eric Klinger
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.)
Safran Aircraft Engines SAS
Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
SNECMA 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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Publication of DE69914987D1 publication Critical patent/DE69914987D1/de
Application granted granted Critical
Publication of DE69914987T2 publication Critical patent/DE69914987T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03HPRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03H1/00Using plasma to produce a reactive propulsive thrust
    • F03H1/0037Electrostatic ion thrusters
    • F03H1/0062Electrostatic ion thrusters grid-less with an applied magnetic field
    • F03H1/0075Electrostatic ion thrusters grid-less with an applied magnetic field with an annular channel; Hall-effect thrusters with closed electron drift
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03HPRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03H1/00Using plasma to produce a reactive propulsive thrust
    • F03H1/0006Details applicable to different types of plasma thrusters
    • F03H1/0031Thermal management, heating or cooling parts of the thruster
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05HPLASMA TECHNIQUE; PRODUCTION OF ACCELERATED ELECTRICALLY-CHARGED PARTICLES OR OF NEUTRONS; PRODUCTION OR ACCELERATION OF NEUTRAL MOLECULAR OR ATOMIC BEAMS
    • H05H1/00Generating plasma; Handling plasma
    • H05H1/54Plasma 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)
DE69914987T 1998-08-25 1999-08-04 Auf hohen thermischen Belastungen abgestimmter Plasmamotor mit geschlossenem Elektronendrift Expired - Lifetime DE69914987T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9810674A FR2782884B1 (fr) 1998-08-25 1998-08-25 Propulseur a plasma a derive fermee d'electrons adapte a de fortes charges thermiques
FR9810674 1998-08-25

Publications (2)

Publication Number Publication Date
DE69914987D1 true DE69914987D1 (de) 2004-04-01
DE69914987T2 DE69914987T2 (de) 2004-12-16

Family

ID=9529859

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69914987T Expired - Lifetime DE69914987T2 (de) 1998-08-25 1999-08-04 Auf hohen thermischen Belastungen abgestimmter Plasmamotor mit geschlossenem Elektronendrift

Country Status (9)

Country Link
US (1) US6281622B1 (de)
EP (1) EP0982976B1 (de)
JP (1) JP4347461B2 (de)
CA (1) CA2280479C (de)
DE (1) DE69914987T2 (de)
FR (1) FR2782884B1 (de)
IL (1) IL131182A (de)
RU (1) RU2219371C2 (de)
UA (1) UA57770C2 (de)

Families Citing this family (39)

* Cited by examiner, † Cited by third party
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DE10014033C2 (de) * 2000-03-22 2002-01-24 Thomson Tubes Electroniques Gm Plasma-Beschleuniger-Anordnung
US6448721B2 (en) * 2000-04-14 2002-09-10 General Plasma Technologies Llc Cylindrical geometry hall thruster
FR2842261A1 (fr) * 2002-07-09 2004-01-16 Centre Nat Etd Spatiales Propulseur plasmique a effet hall
US7461502B2 (en) 2003-03-20 2008-12-09 Elwing Llc Spacecraft thruster
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
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
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
FR2919755B1 (fr) * 2007-08-02 2017-05-05 Centre Nat De La Rech Scient (C N R S ) Dispositif d'ejection d'electrons a effet hall
DE102007062150A1 (de) * 2007-09-14 2009-04-02 Thales Electron Devices Gmbh Vorrichtung zur Ableitung von Verlustwärme sowie Ionenbeschleunigeranordnung und Wanderfeldröhrenanordnung mit einer Wärmeleitanordnung
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
JP5295423B2 (ja) * 2010-03-01 2013-09-18 三菱電機株式会社 ホールスラスタ及び宇宙航行体及び推進方法
RU2447625C2 (ru) * 2010-03-22 2012-04-10 Федеральное государственное унитарное предприятие "Опытное конструкторское бюро "Факел" Плазменный ускоритель с замкнутым дрейфом электронов
FR2976029B1 (fr) 2011-05-30 2016-03-11 Snecma Propulseur a effet hall
FR2979956B1 (fr) 2011-09-09 2013-09-27 Snecma Systeme de propulsion electrique a propulseurs a plasma stationnaire
US8575565B2 (en) * 2011-10-10 2013-11-05 Guardian Industries Corp. Ion source apparatus and methods of using the same
RU2504683C1 (ru) * 2012-06-22 2014-01-20 Михаил Никитович Алексенко Способ управления вектором тяги реактивного двигателя летательного аппарата
RU2527798C2 (ru) * 2012-11-28 2014-09-10 Михаил Никитович Алексенко Устройство управления вектором тяги реактивного двигателя
RU2523427C1 (ru) * 2012-12-28 2014-07-20 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Московский государственный технический университет имени Н.Э. Баумана" (МГТУ им. Н.Э. Баумана) Способ формирования компактного плазмоида
RU2524571C1 (ru) * 2013-01-22 2014-07-27 Объединенный Институт Ядерных Исследований Индукционный циклический ускоритель электронов
RU2527898C1 (ru) * 2013-04-17 2014-09-10 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Московский государственный технический университет радиотехники, электроники и автоматики" Стационарный плазменный двигатель малой мощности
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
RU2568825C2 (ru) * 2014-03-24 2015-11-20 Акционерное общество "Научно-исследовательский институт электромеханики" (АО "НИИЭМ") Электрореактивная двигательная установка
US9642239B2 (en) 2015-04-17 2017-05-02 Fermi Research Alliance, Llc Conduction cooling systems for linear accelerator cavities
RU2620442C2 (ru) * 2015-05-29 2017-05-25 Открытое акционерное общество "ОКБ-Планета" ОАО "ОКБ-Планета" Источник ионов
CN105163475A (zh) * 2015-08-03 2015-12-16 兰州空间技术物理研究所 一种离子推力器放电室双向气体供给装置
US20180255632A1 (en) * 2015-12-10 2018-09-06 Halliburton Energy Services, Inc. Downhole field ionization neutron generator
RU167315U1 (ru) * 2016-10-11 2017-01-10 Федеральное государственное бюджетное образовательное учреждение высшего образования "Московский технологический университет" (МИРЭА) Стационарный плазменный двигатель малой мощности
CN107795445B (zh) * 2017-09-01 2019-08-23 兰州空间技术物理研究所 一种环形磁钢环切场离子推力器结构和主支撑环
US10932355B2 (en) 2017-09-26 2021-02-23 Jefferson Science Associates, Llc High-current conduction cooled superconducting radio-frequency cryomodule
CN109779863B (zh) * 2019-01-31 2020-06-23 哈尔滨工业大学 一种霍尔推力器安装支架
RU2724375C1 (ru) * 2019-12-24 2020-06-23 Николай Борисович Болотин Ионный ракетный двигатель и способ его работы
RU2735043C1 (ru) * 2020-05-20 2020-10-27 Николай Борисович Болотин Плазменно-ионный ракетный двигатель
CN112017840B (zh) * 2020-08-11 2021-12-07 北京控制工程研究所 一种低功率霍尔推力器用磁屏及固定结构
WO2023038611A1 (ru) * 2021-09-13 2023-03-16 Частное Акционерное Общество "Фэд" Стационарный ионно-плазменный двигатель
CN114352831A (zh) * 2021-12-21 2022-04-15 上海空间推进研究所 气体分配器
WO2023244857A1 (en) * 2022-06-17 2023-12-21 The Regents Of The University Of Michigan Hall thruster

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE69207720T2 (de) * 1991-11-04 1996-05-30 Fakel Enterprise Plasmabeschleuniger mit geschlossener Elektronenlaufbahn
FR2693770B1 (fr) * 1992-07-15 1994-10-14 Europ Propulsion Moteur à plasma à dérive fermée d'électrons.
US5763989A (en) * 1995-03-16 1998-06-09 Front Range Fakel, Inc. Closed drift ion source with improved magnetic field
FR2743191B1 (fr) * 1995-12-29 1998-03-27 Europ Propulsion Source d'ions a derive fermee d'electrons
US6158209A (en) * 1997-05-23 2000-12-12 Societe Nationale D'etude Et De Construction De Moteurs D'aviation-S.N.E.C.M.A. Device for concentrating ion beams for hydromagnetic propulsion means and hydromagnetic propulsion means equipped with same
US6208080B1 (en) * 1998-06-05 2001-03-27 Primex Aerospace Company Magnetic flux shaping in ion accelerators with closed electron drift

Also Published As

Publication number Publication date
UA57770C2 (uk) 2003-07-15
CA2280479C (en) 2007-10-23
DE69914987T2 (de) 2004-12-16
FR2782884B1 (fr) 2000-11-24
JP4347461B2 (ja) 2009-10-21
IL131182A (en) 2003-06-24
IL131182A0 (en) 2001-01-28
JP2000073937A (ja) 2000-03-07
EP0982976A1 (de) 2000-03-01
FR2782884A1 (fr) 2000-03-03
US6281622B1 (en) 2001-08-28
RU2219371C2 (ru) 2003-12-20
EP0982976B1 (de) 2004-02-25
CA2280479A1 (en) 2000-02-25

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