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GB0027739D0 - Plasmajet - Google Patents

Plasmajet

Info

Publication number
GB0027739D0
GB0027739D0 GB0027739A GB0027739A GB0027739D0 GB 0027739 D0 GB0027739 D0 GB 0027739D0 GB 0027739 A GB0027739 A GB 0027739A GB 0027739 A GB0027739 A GB 0027739A GB 0027739 D0 GB0027739 D0 GB 0027739D0
Authority
GB
United Kingdom
Prior art keywords
plasmajet
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.)
Withdrawn
Application number
GB0027739A
Other versions
GB2358043A (en
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.)
Polyflex Aerospace Ltd
Original Assignee
Polyflex Aerospace Ltd
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 Polyflex Aerospace Ltd filed Critical Polyflex Aerospace Ltd
Publication of GB0027739D0 publication Critical patent/GB0027739D0/en
Publication of GB2358043A publication Critical patent/GB2358043A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01J—ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J27/00—Ion beam tubes
    • H01J27/02—Ion sources; Ion guns
    • H01J27/028—Negative ion sources
    • 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)
GB0027739A 1999-11-17 2000-11-14 Deriving thrust by accelerating charged particles Withdrawn GB2358043A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GBGB9927053.0A GB9927053D0 (en) 1999-11-17 1999-11-17 Plasmajet

Publications (2)

Publication Number Publication Date
GB0027739D0 true GB0027739D0 (en) 2000-12-27
GB2358043A GB2358043A (en) 2001-07-11

Family

ID=10864587

Family Applications (2)

Application Number Title Priority Date Filing Date
GBGB9927053.0A Ceased GB9927053D0 (en) 1999-11-17 1999-11-17 Plasmajet
GB0027739A Withdrawn GB2358043A (en) 1999-11-17 2000-11-14 Deriving thrust by accelerating charged particles

Family Applications Before (1)

Application Number Title Priority Date Filing Date
GBGB9927053.0A Ceased GB9927053D0 (en) 1999-11-17 1999-11-17 Plasmajet

Country Status (1)

Country Link
GB (2) GB9927053D0 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1604110B1 (en) 2003-03-05 2013-05-15 Thales Air Systems & Electron Devices GmbH Ion thruster pertaining to a spacecraft and method for controlling the position of a spacecraft comprising one such ion thruster
PT106150A (en) * 2012-02-14 2013-08-14 Alexandre Tiago Batista De Alves Martins ELECTROMAGNETIC PROPULSION SYSTEM
CN114718830B (en) * 2022-04-13 2024-05-10 哈尔滨工业大学 Working medium-free annular hot wire cathode

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3122882A (en) * 1960-11-23 1964-03-03 Aerojet General Co Propulsion means
FR1376507A (en) * 1963-04-29 1964-10-31 Commissariat Energie Atomique Ionized gas accelerator and devices including application
US3969646A (en) * 1975-02-10 1976-07-13 Ion Tech, Inc. Electron-bombardment ion source including segmented anode of electrically conductive, magnetic material
US4825646A (en) * 1987-04-23 1989-05-02 Hughes Aircraft Company Spacecraft with modulated thrust electrostatic ion thruster and associated method
US5780862A (en) * 1994-01-11 1998-07-14 Siess; Harold E. Method and apparatus for generating ions
US5646476A (en) * 1994-12-30 1997-07-08 Electric Propulsion Laboratory, Inc. Channel ion source
AU5423096A (en) * 1996-03-15 1997-10-01 Alfred Y. Wong High-altitude lighter-than-air stationary platforms including ion engines

Also Published As

Publication number Publication date
GB9927053D0 (en) 2000-01-12
GB2358043A (en) 2001-07-11

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)