JPS55134767A - Electronic impulse type ion engine - Google Patents

Electronic impulse type ion engine

Info

Publication number
JPS55134767A
JPS55134767A JP4080479A JP4080479A JPS55134767A JP S55134767 A JPS55134767 A JP S55134767A JP 4080479 A JP4080479 A JP 4080479A JP 4080479 A JP4080479 A JP 4080479A JP S55134767 A JPS55134767 A JP S55134767A
Authority
JP
Japan
Prior art keywords
anode
electron
discharge chamber
plasma
void
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.)
Pending
Application number
JP4080479A
Other languages
Japanese (ja)
Inventor
Tadanori Shimada
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.)
Mitsubishi Electric Corp
Original Assignee
Mitsubishi Electric Corp
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 Mitsubishi Electric Corp filed Critical Mitsubishi Electric Corp
Priority to JP4080479A priority Critical patent/JPS55134767A/en
Publication of JPS55134767A publication Critical patent/JPS55134767A/en
Pending legal-status Critical Current

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  • Electron Sources, Ion Sources (AREA)

Abstract

PURPOSE: To uniform ion density and electron density of plasma produced in a discharge chamber and also to decrease consumption power necessary for the formation of plasma by impressing variant potentials to a plural anode groups.
CONSTITUTION: An electron released from a source 1 is accelerated for radial diffusion in a discharge chamber by an electric field of the first anode 6. In a void between the first anode 6 and the second anode 7, diffusion of the electron turns to a focusing direction according to a lens action of the electric field, and further the direction of the electron is again corrected in the same way in a void between the second anode 7 and the third anode 8. In the discharge chamber, the electron released from the source 1 moves spirally along a flying route 14 of the electron by a magnetic field 13, collides with a neutral atom in a gas 12 effuciently to ionize the gas 12, thus producing a uniform plasma in the discharge chamber.
COPYRIGHT: (C)1980,JPO&Japio
JP4080479A 1979-04-04 1979-04-04 Electronic impulse type ion engine Pending JPS55134767A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP4080479A JPS55134767A (en) 1979-04-04 1979-04-04 Electronic impulse type ion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP4080479A JPS55134767A (en) 1979-04-04 1979-04-04 Electronic impulse type ion engine

Publications (1)

Publication Number Publication Date
JPS55134767A true JPS55134767A (en) 1980-10-20

Family

ID=12590817

Family Applications (1)

Application Number Title Priority Date Filing Date
JP4080479A Pending JPS55134767A (en) 1979-04-04 1979-04-04 Electronic impulse type ion engine

Country Status (1)

Country Link
JP (1) JPS55134767A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS62178779A (en) * 1986-01-30 1987-08-05 Toshiba Corp Rf type ion thruster
JPH02502473A (en) * 1987-12-11 1990-08-09 ヒユーズ・エアクラフト・カンパニー Electrostatic ion attitude control engine with improved propulsion control
CN104061137A (en) * 2014-07-11 2014-09-24 哈尔滨工业大学 Method for correcting on-rail flight hall thruster thrust parameters according to ground experiment parameters
GB2588415A (en) * 2019-10-22 2021-04-28 Gaston Klemz Nicholas An apparatus for generating a force

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS62178779A (en) * 1986-01-30 1987-08-05 Toshiba Corp Rf type ion thruster
JPH07101029B2 (en) * 1986-01-30 1995-11-01 株式会社東芝 RF type ion thruster
JPH02502473A (en) * 1987-12-11 1990-08-09 ヒユーズ・エアクラフト・カンパニー Electrostatic ion attitude control engine with improved propulsion control
CN104061137A (en) * 2014-07-11 2014-09-24 哈尔滨工业大学 Method for correcting on-rail flight hall thruster thrust parameters according to ground experiment parameters
CN104061137B (en) * 2014-07-11 2016-10-05 哈尔滨工业大学 Method according to ground experiment parameter correction flight hall thruster thrust parameter in-orbit
GB2588415A (en) * 2019-10-22 2021-04-28 Gaston Klemz Nicholas An apparatus for generating a force
WO2021079090A1 (en) * 2019-10-22 2021-04-29 Klemz Nicholas Gaston An apparatus for generating a force

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