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RU2002125111A - PLASMA ACCELERATOR - Google Patents

PLASMA ACCELERATOR

Info

Publication number
RU2002125111A
RU2002125111A RU2002125111/06A RU2002125111A RU2002125111A RU 2002125111 A RU2002125111 A RU 2002125111A RU 2002125111/06 A RU2002125111/06 A RU 2002125111/06A RU 2002125111 A RU2002125111 A RU 2002125111A RU 2002125111 A RU2002125111 A RU 2002125111A
Authority
RU
Russia
Prior art keywords
plasma
longitudinal axis
chamber
accelerator according
plasma accelerator
Prior art date
Application number
RU2002125111/06A
Other languages
Russian (ru)
Other versions
RU2239962C2 (en
Inventor
Гюнтер КОРНФЕЛД
Вернер СЧВЕРТФЕГЕР
Original Assignee
Тайлес Електрон Девайсез Гмбх
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
Priority claimed from DE10014034A external-priority patent/DE10014034C2/en
Application filed by Тайлес Електрон Девайсез Гмбх filed Critical Тайлес Електрон Девайсез Гмбх
Publication of RU2002125111A publication Critical patent/RU2002125111A/en
Application granted granted Critical
Publication of RU2239962C2 publication Critical patent/RU2239962C2/en

Links

Claims (6)

1. Плазменный ускоритель с плазменной камерой вокруг продольной оси, электродной установкой, создающей электрическую разность потенциалов в качестве поля разгона для положительно заряженных ионов на участке разгона параллельно продольной оси, и имеющего устройство, подающее сфокусированный пучок электронов в плазменную камеру и управляемый с помощью магнитной системы, плазменная камера кольцеобразной формы вокруг продольной оси с радиальными внутренними и внешними стенками, пучок электронов подается в виде полого цилиндрического пучка.1. Plasma accelerator with a plasma chamber around the longitudinal axis, an electrode installation that creates an electric potential difference as an acceleration field for positively charged ions in the acceleration region parallel to the longitudinal axis, and having a device that delivers a focused electron beam into the plasma chamber and controlled by a magnetic system , a plasma chamber of an annular shape around a longitudinal axis with radial internal and external walls, the electron beam is supplied in the form of a hollow cylindrical PFA. 2. Плазменный ускоритель по п.1, отличающийся по отношению к плазменной камере тем, что магнитная система имеет радиально внутренние и внешние магнитные устройства.2. The plasma accelerator according to claim 1, characterized in relation to the plasma chamber in that the magnetic system has radially internal and external magnetic devices. 3. Плазменный ускоритель по п.1 или 2, отличающийся тем, что магнитная система также имеет тороидальную структуру.3. The plasma accelerator according to claim 1 or 2, characterized in that the magnetic system also has a toroidal structure. 4. Плазменный ускоритель по одному из пп.1-3, отличающийся тем, что в продольном направлении по длине плазменной камеры по меньшей мере одно промежуточное электродное устройство имеет первую часть электрода с расположением на внешней стенке камеры, а вторую часть с расположением напротив на внутренней стенке камеры вокруг продольной оси, этот электрод находится под воздействием промежуточного потенциала разности потенциалов.4. Plasma accelerator according to one of claims 1 to 3, characterized in that in the longitudinal direction along the length of the plasma chamber, at least one intermediate electrode device has a first electrode part with an arrangement on the outer wall of the chamber, and a second part with an opposite arrangement on the inner the chamber wall around the longitudinal axis, this electrode is under the influence of an intermediate potential of the potential difference. 5. Плазменный ускоритель по одному из пп.1-4, отличающийся тем, что его магнитная система состоит из нескольких последовательных магнитных установок, разделенных между собой параллельно продольной оси, и имеет противоположно установленные полюса в продольном направлении.5. Plasma accelerator according to one of claims 1 to 4, characterized in that its magnetic system consists of several consecutive magnetic installations, separated from each other parallel to the longitudinal axis, and has opposite poles in the longitudinal direction. 6. Плазменный ускоритель по п.4 или 5, отличающийся тем, что по меньшей мере один промежуточный электрод частично или полностью перекрывает пространство между соседними полюсами магнитного устройства.6. The plasma accelerator according to claim 4 or 5, characterized in that at least one intermediate electrode partially or completely overlaps the space between adjacent poles of the magnetic device.
RU2002125111/06A 2000-03-22 2001-03-22 Plasma accelerator RU2239962C2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE10014034A DE10014034C2 (en) 2000-03-22 2000-03-22 Plasma accelerator arrangement
DE10014034.3 2000-03-22

Publications (2)

Publication Number Publication Date
RU2002125111A true RU2002125111A (en) 2004-04-20
RU2239962C2 RU2239962C2 (en) 2004-11-10

Family

ID=7635807

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2002125111/06A RU2239962C2 (en) 2000-03-22 2001-03-22 Plasma accelerator

Country Status (11)

Country Link
US (1) US6798141B2 (en)
EP (1) EP1269803B1 (en)
JP (1) JP4944336B2 (en)
KR (1) KR20030014373A (en)
CN (1) CN1418453A (en)
AT (1) ATE408978T1 (en)
AU (1) AU6004801A (en)
DE (2) DE10014034C2 (en)
ES (1) ES2312434T3 (en)
RU (1) RU2239962C2 (en)
WO (1) WO2001072093A2 (en)

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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
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US8016246B2 (en) * 2007-05-25 2011-09-13 The Boeing Company Plasma actuator system and method for use with a weapons bay on a high speed mobile platform
US8016247B2 (en) * 2007-05-25 2011-09-13 The Boeing Company Plasma flow control actuator system and method
WO2011011049A2 (en) * 2009-07-20 2011-01-27 The Board Of Trustees Of The Leland Stanford Junior University Method and apparatus for inductive amplification of ion beam energy
US9089040B2 (en) * 2010-03-01 2015-07-21 Mitsubishi Electric Corporation Hall thruster, cosmonautic vehicle, and propulsion method
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RU2500046C2 (en) * 2011-04-05 2013-11-27 Геннадий Викторович Карпов Method of obtaining accelerated ions in neutron tubes and apparatus for realising said method
US20130026917A1 (en) * 2011-07-29 2013-01-31 Walker Mitchell L R Ion focusing in a hall effect thruster
RU2517184C2 (en) * 2012-05-18 2014-05-27 Федеральное государственное бюджетное учреждение науки Институт общей физики им. А.М. Прохорова Российской академии наук Method for controlled collective acceleration of electron-ion bunches
KR101420716B1 (en) * 2012-05-23 2014-07-22 성균관대학교산학협력단 A cyclotron
CN103037609B (en) * 2013-01-10 2014-12-31 哈尔滨工业大学 Jet Plasma Electronic Energy Conditioner
CN104001270B (en) * 2014-05-07 2016-07-06 上海交通大学 Extrahigh energy electron beam or photon beam radiation treatment robot system
US10428806B2 (en) * 2016-01-22 2019-10-01 The Boeing Company Structural Propellant for ion rockets (SPIR)
CN108915969B (en) * 2018-07-18 2020-09-22 北京理工大学 Multi-mode helical wave ion thruster
CN111111581B (en) * 2019-12-19 2021-07-02 中国科学院电工研究所 A plasma fuel reformer

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