GB1039824A - Ion beam propulsion systems - Google Patents
Ion beam propulsion systemsInfo
- Publication number
- GB1039824A GB1039824A GB16817/64A GB1681764A GB1039824A GB 1039824 A GB1039824 A GB 1039824A GB 16817/64 A GB16817/64 A GB 16817/64A GB 1681764 A GB1681764 A GB 1681764A GB 1039824 A GB1039824 A GB 1039824A
- Authority
- GB
- United Kingdom
- Prior art keywords
- electrode
- ion beam
- secondary emissive
- cross
- neutralization
- 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.)
- Expired
Links
- 238000010884 ion-beam technique Methods 0.000 title abstract 3
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 abstract 2
- 238000006386 neutralization reaction Methods 0.000 abstract 2
- 229910052786 argon Inorganic materials 0.000 abstract 1
- 229910052792 caesium Inorganic materials 0.000 abstract 1
- TVFDJXOCXUVLDH-UHFFFAOYSA-N caesium atom Chemical compound [Cs] TVFDJXOCXUVLDH-UHFFFAOYSA-N 0.000 abstract 1
- 150000002500 ions Chemical class 0.000 abstract 1
- 239000000463 material Substances 0.000 abstract 1
- 238000012986 modification Methods 0.000 abstract 1
- 230000004048 modification Effects 0.000 abstract 1
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 abstract 1
- 229910052721 tungsten Inorganic materials 0.000 abstract 1
- 239000010937 tungsten Substances 0.000 abstract 1
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
- F03H1/0006—Details applicable to different types of plasma thrusters
- F03H1/0025—Neutralisers, i.e. means for keeping electrical neutrality
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/40—Arrangements or adaptations of propulsion systems
- B64G1/405—Ion or plasma engines
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01J—ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
- H01J27/00—Ion beam tubes
- H01J27/02—Ion sources; Ion guns
- H01J27/022—Details
- H01J27/024—Extraction optics, e.g. grids
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01J—ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
- H01J43/00—Secondary-emission tubes; Electron-multiplier tubes
- H01J43/02—Tubes in which one or a few electrodes are secondary-electron emitting electrodes
Abstract
1,039,824. Ion beam space propulsion engine. CSF-COMPAGNIE GENERALE DE TELEGRAPHIE SANS FIL. April 23,1964 [May 21, 1963], No. 16817/64. Class F1J. [Also in Group H1] In an ion beam space propulsion engine neutralization is effected by secondary electron emission, the outer part of the beam 28, after being concentrated to a cross-over point or to a region of minimum cross-section 31 by an electrostatic lens system 24, 29, 32 diverges onto a secondary emissive surface 33 within the electrode 32. By adjusting the position of the cross-over the degree of neutralization may be varied. Alternatively a magnetic lens may be used and in modifications the secondary emissive surface may be provided on an outwardly flared portion of the electrode 32 or the electrode 32 may be terminated by a secondary emissive grid of constant or radially variable pitch. A suitable secondary emissive material is tungsten and the ion may be produced from caesium or argon vapour.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR933389A FR1366023A (en) | 1963-05-02 | 1963-05-02 | Improvements to neutralized ion beam propulsion devices |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1039824A true GB1039824A (en) | 1966-08-24 |
Family
ID=8802874
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB16817/64A Expired GB1039824A (en) | 1963-05-02 | 1964-04-23 | Ion beam propulsion systems |
Country Status (4)
Country | Link |
---|---|
US (1) | US3363124A (en) |
FR (1) | FR1366023A (en) |
GB (1) | GB1039824A (en) |
NL (1) | NL6404832A (en) |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3448315A (en) * | 1966-10-11 | 1969-06-03 | Itt | Ion gun improvements for operation in the micron pressure range and utilizing a diffuse discharge |
US3546513A (en) * | 1968-03-11 | 1970-12-08 | Us Air Force | High yield ion source |
FR2061809A5 (en) * | 1969-04-04 | 1971-06-25 | Commissariat Energie Atomique | |
US3845300A (en) * | 1973-04-18 | 1974-10-29 | Atomic Energy Commission | Apparatus and method for magnetoplasmadynamic isotope separation |
US4463255A (en) * | 1980-09-24 | 1984-07-31 | Varian Associates, Inc. | Apparatus for enhanced neutralization of positively charged ion beam |
EP0104818A3 (en) * | 1982-09-29 | 1985-10-23 | Eaton Corporation | Ion implantation device |
JPS6043620B2 (en) * | 1982-11-25 | 1985-09-28 | 日新ハイボルテージ株式会社 | microwave ion source |
US4713542A (en) * | 1984-10-31 | 1987-12-15 | United States Of America As Represented By The Secretary Of The Navy | Ton beam neutralizer |
JPS6410563A (en) * | 1987-07-02 | 1989-01-13 | Sumitomo Eaton Nova | Electric charging suppressor of ion implanter |
US4933546A (en) * | 1988-08-23 | 1990-06-12 | Grumman Aerospace Corporation | Orifice ring ion beam neutralizer |
US5136171A (en) * | 1990-03-02 | 1992-08-04 | Varian Associates, Inc. | Charge neutralization apparatus for ion implantation system |
US6158209A (en) * | 1997-05-23 | 2000-12-12 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation-S.N.E.C.M.A. | Device for concentrating ion beams for hydromagnetic propulsion means and hydromagnetic propulsion means equipped with same |
US10714307B2 (en) * | 2018-06-08 | 2020-07-14 | Kla-Tencor Corporation | Neutral atom imaging system |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3014154A (en) * | 1959-10-01 | 1961-12-19 | Kenneth W Ehlers | Ion rocket engine |
-
1963
- 1963-05-02 FR FR933389A patent/FR1366023A/en not_active Expired
-
1964
- 1964-04-15 US US359960A patent/US3363124A/en not_active Expired - Lifetime
- 1964-04-23 GB GB16817/64A patent/GB1039824A/en not_active Expired
- 1964-05-01 NL NL6404832A patent/NL6404832A/xx unknown
Also Published As
Publication number | Publication date |
---|---|
NL6404832A (en) | 1964-11-03 |
US3363124A (en) | 1968-01-09 |
FR1366023A (en) | 1964-07-10 |
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