IL131182A - Closed electron drift plasma thruster adapted to high thermal loads - Google Patents

Closed electron drift plasma thruster adapted to high thermal loads

Info

Publication number
IL131182A
IL131182A IL13118299A IL13118299A IL131182A IL 131182 A IL131182 A IL 131182A IL 13118299 A IL13118299 A IL 13118299A IL 13118299 A IL13118299 A IL 13118299A IL 131182 A IL131182 A IL 131182A
Authority
IL
Israel
Prior art keywords
high thermal
thermal loads
electron drift
plasma thruster
closed electron
Prior art date
Application number
IL13118299A
Other languages
English (en)
Other versions
IL131182A0 (en
Original Assignee
Snecma
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 Snecma filed Critical Snecma
Publication of IL131182A0 publication Critical patent/IL131182A0/xx
Publication of IL131182A publication Critical patent/IL131182A/xx

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
    • 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
    • F03H1/0006—Details applicable to different types of plasma thrusters
    • F03H1/0031—Thermal management, heating or cooling parts of the thruster
    • 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)
IL13118299A 1998-08-25 1999-07-30 Closed electron drift plasma thruster adapted to high thermal loads IL131182A (en)

Applications Claiming Priority (1)

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

Publications (2)

Publication Number Publication Date
IL131182A0 IL131182A0 (en) 2001-01-28
IL131182A true IL131182A (en) 2003-06-24

Family

ID=9529859

Family Applications (1)

Application Number Title Priority Date Filing Date
IL13118299A IL131182A (en) 1998-08-25 1999-07-30 Closed electron drift plasma thruster adapted to high thermal loads

Country Status (9)

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

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
WO2017099773A1 (fr) * 2015-12-10 2017-06-15 Halliburton Energy Services, Inc. Générateur de neutrons à ionisation de champ de fond
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 (fr) * 2021-09-13 2023-03-16 Частное Акционерное Общество "Фэд" Moteur ionique-plasmique stationnaire
CN114352831A (zh) * 2021-12-21 2022-04-15 上海空间推进研究所 气体分配器
WO2023244857A1 (fr) * 2022-06-17 2023-12-21 The Regents Of The University Of Michigan Propulseur à effet hall

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0541309B1 (fr) * 1991-11-04 1996-01-17 Fakel Enterprise Accélérateur de plasma avec parcours fermé d'électrons
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
EP0914560B1 (fr) * 1997-05-23 2005-08-24 Société Nationale d'Etude et de Construction de Moteurs d' Aviation PROPULSEUR A PLASMA avec DISPOSITIF DE CONCENTRATION DE FAISCEAU D'IONS
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
FR2782884B1 (fr) 2000-11-24
EP0982976B1 (fr) 2004-02-25
CA2280479C (fr) 2007-10-23
JP2000073937A (ja) 2000-03-07
RU2219371C2 (ru) 2003-12-20
FR2782884A1 (fr) 2000-03-03
US6281622B1 (en) 2001-08-28
JP4347461B2 (ja) 2009-10-21
IL131182A0 (en) 2001-01-28
CA2280479A1 (fr) 2000-02-25
UA57770C2 (uk) 2003-07-15
DE69914987T2 (de) 2004-12-16
EP0982976A1 (fr) 2000-03-01
DE69914987D1 (de) 2004-04-01

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