AU4818699A - Magnetic flux shaping in ion accelerators with closed electron drift - Google Patents

Magnetic flux shaping in ion accelerators with closed electron drift

Info

Publication number
AU4818699A
AU4818699A AU48186/99A AU4818699A AU4818699A AU 4818699 A AU4818699 A AU 4818699A AU 48186/99 A AU48186/99 A AU 48186/99A AU 4818699 A AU4818699 A AU 4818699A AU 4818699 A AU4818699 A AU 4818699A
Authority
AU
Australia
Prior art keywords
magnetic flux
electron drift
ion accelerators
closed electron
flux shaping
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.)
Abandoned
Application number
AU48186/99A
Inventor
Randall S. Aadland
Kristi H. De Grys
David Q. King
Dennis L. Tilley
Arnold W. Voigt
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.)
Primex Aerospace Co
Original Assignee
Primex Aerospace Co
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 US09/191,749 external-priority patent/US6208080B1/en
Application filed by Primex Aerospace Co filed Critical Primex Aerospace Co
Publication of AU4818699A publication Critical patent/AU4818699A/en
Abandoned 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

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)
  • Plasma Technology (AREA)
  • Particle Accelerators (AREA)
AU48186/99A 1998-06-05 1999-06-03 Magnetic flux shaping in ion accelerators with closed electron drift Abandoned AU4818699A (en)

Applications Claiming Priority (7)

Application Number Priority Date Filing Date Title
US8816498P 1998-06-05 1998-06-05
US60088164 1998-06-05
US9226998P 1998-07-10 1998-07-10
US60092269 1998-07-10
US09/191,749 US6208080B1 (en) 1998-06-05 1998-11-13 Magnetic flux shaping in ion accelerators with closed electron drift
US09191749 1998-11-13
PCT/US1999/012402 WO1999063221A2 (en) 1998-06-05 1999-06-03 Magnetic flux shaping in ion accelerators with closed electron drift

Publications (1)

Publication Number Publication Date
AU4818699A true AU4818699A (en) 1999-12-20

Family

ID=27375907

Family Applications (1)

Application Number Title Priority Date Filing Date
AU48186/99A Abandoned AU4818699A (en) 1998-06-05 1999-06-03 Magnetic flux shaping in ion accelerators with closed electron drift

Country Status (6)

Country Link
EP (1) EP1082540B1 (en)
JP (1) JP4294867B2 (en)
AU (1) AU4818699A (en)
DE (1) DE69902589T2 (en)
IL (1) IL139487A (en)
WO (1) WO1999063221A2 (en)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2857555B1 (en) * 2003-07-09 2005-10-14 Snecma Moteurs PLASMA ACCELERATOR WITH CLOSED ELECTRON DERIVATIVE
JP2006147449A (en) 2004-11-24 2006-06-08 Japan Aerospace Exploration Agency High-frequency discharge plasma generation type two-step hole effect plasma accelerator
JP4816004B2 (en) * 2005-10-28 2011-11-16 三菱電機株式会社 Hall thrusters and spacecraft
JP4650258B2 (en) 2005-12-27 2011-03-16 三菱電機株式会社 Power supply
JP4816179B2 (en) * 2006-03-20 2011-11-16 三菱電機株式会社 Hall thruster
RU2458490C2 (en) * 2008-02-28 2012-08-10 Федеральное государственное унитарное предприятие "Центральный научно-исследовательский институт машиностроения" (ФГУП ЦНИИмаш) Method of controlling ion electric rocket engines and apparatus for realising said method (versions)
FR2941503B1 (en) * 2009-01-27 2011-03-04 Snecma PROPELLER WITH CLOSED DERIVATIVE ELECTRON
JP2011144699A (en) * 2010-01-12 2011-07-28 Mitsubishi Electric Corp Electric power supply device
KR101403101B1 (en) * 2012-10-17 2014-06-03 주식회사 포스코 Linear ion beam source

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
IL126413A0 (en) * 1996-04-01 1999-05-09 Int Scient Products A hall effect plasma accelerator

Also Published As

Publication number Publication date
DE69902589D1 (en) 2002-09-26
WO1999063221A2 (en) 1999-12-09
IL139487A0 (en) 2001-11-25
EP1082540A2 (en) 2001-03-14
IL139487A (en) 2004-02-19
DE69902589T2 (en) 2003-05-22
WO1999063221A3 (en) 2000-02-24
JP2002517661A (en) 2002-06-18
JP4294867B2 (en) 2009-07-15
EP1082540B1 (en) 2002-08-21

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Legal Events

Date Code Title Description
MK6 Application lapsed section 142(2)(f)/reg. 8.3(3) - pct applic. not entering national phase