GB916353A - Improvements in or relating to apparatus for generating an ion beam - Google Patents
Improvements in or relating to apparatus for generating an ion beamInfo
- Publication number
- GB916353A GB916353A GB28827/60A GB2882760A GB916353A GB 916353 A GB916353 A GB 916353A GB 28827/60 A GB28827/60 A GB 28827/60A GB 2882760 A GB2882760 A GB 2882760A GB 916353 A GB916353 A GB 916353A
- Authority
- GB
- United Kingdom
- Prior art keywords
- see group
- xxvi
- ion beams
- relating
- generating
- 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
- 238000007599 discharging Methods 0.000 abstract 1
- 230000005611 electricity Effects 0.000 abstract 1
- 239000003380 propellant Substances 0.000 abstract 1
- 230000003068 static effect Effects 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
- F03H1/0037—Electrostatic ion thrusters
- F03H1/0056—Electrostatic ion thrusters with an acceleration grid and an applied magnetic field
-
- 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
-
- 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
- B64G1/411—Electric propulsion
- B64G1/413—Ion or plasma engines
-
- 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
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)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Electron Sources, Ion Sources (AREA)
- Particle Accelerators (AREA)
Abstract
916,353. Discharging static electricity. UNITED STATES ATOMIC ENERGY COMMISSION. Aug. 19, 1960 [Oct. 1, 1959], No. 28827/60. Drawings to Specification. Class 35. [Also in Groups XXVI and XL (a)] In an ion rocket engine (see Group XXVI) in which propellant is forced through heated porous electrodes where it is ionized by contact and is then accelerated as positive ion beams (see Group XL (a)) the ion beams, and hence the rocket casing, are neutralized by electrons injected from directly or indirectly heated cathodes or from secondary-electron emissive electrodes.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US843898A US3014154A (en) | 1959-10-01 | 1959-10-01 | Ion rocket engine |
Publications (1)
Publication Number | Publication Date |
---|---|
GB916353A true GB916353A (en) | 1963-01-23 |
Family
ID=25291277
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB28827/60A Expired GB916353A (en) | 1959-10-01 | 1960-08-19 | Improvements in or relating to apparatus for generating an ion beam |
Country Status (2)
Country | Link |
---|---|
US (1) | US3014154A (en) |
GB (1) | GB916353A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1233340B (en) * | 1963-05-02 | 1967-01-26 | Csf | Electric recoil drive with an ion source |
Families Citing this family (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3212974A (en) * | 1959-06-23 | 1965-10-19 | Csf | Particle injecting device |
US3138919A (en) * | 1960-06-28 | 1964-06-30 | Alexander T Deutsch | Electrodynamic system |
US3119232A (en) * | 1960-10-04 | 1964-01-28 | Edward A Richley | Rocket engine |
US3369148A (en) * | 1961-07-05 | 1968-02-13 | William J. Hitchcock | System for mixing opposite polarity ions on magnetic field axis |
US3156090A (en) * | 1961-09-18 | 1964-11-10 | Harold R Kaufman | Ion rocket |
US3177654A (en) * | 1961-09-26 | 1965-04-13 | Ryan Aeronautical Company | Electric aerospace propulsion system |
US3102384A (en) * | 1961-12-29 | 1963-09-03 | Willard H Bennett | Propulsion means for space vehicles |
US3201635A (en) * | 1962-03-07 | 1965-08-17 | Arlen F Carter | Method and apparatus for producing a plasma |
US3258909A (en) * | 1962-05-11 | 1966-07-05 | United Aircraft Corp | Direct heating contact ionization propulsion system |
US3210926A (en) * | 1962-06-18 | 1965-10-12 | Trw Inc | Ionic propulsion systems |
US3159967A (en) * | 1963-03-12 | 1964-12-08 | James E Webb | Variable thrust ion engine utilizing thermally decomposable solid fuel |
FR1366023A (en) * | 1963-05-02 | 1964-07-10 | Csf | Improvements to neutralized ion beam propulsion devices |
US3308622A (en) * | 1964-07-29 | 1967-03-14 | Electro Optical Systems Inc | Ion propulsion system with ion engine utilizing power supply hot surface |
US3371489A (en) * | 1964-10-23 | 1968-03-05 | Hughes Aircraft Co | Porous-plug low work-function film cathodes for electron-bombardment ion thrustors |
US3465522A (en) * | 1965-03-09 | 1969-09-09 | Hughes Aircraft Co | Ion rocket |
US3354644A (en) * | 1965-06-08 | 1967-11-28 | Electro Optical Systems Inc | Liquid protection of electrodes |
US3304718A (en) * | 1965-08-04 | 1967-02-21 | James E Webb | Double optic system for ion engine |
US3535880A (en) * | 1966-06-14 | 1970-10-27 | Hughes Aircraft Co | Ion beam deflection system |
JPS53135071A (en) * | 1977-04-28 | 1978-11-25 | Metallgesellschaft Ag | Electric dust collector for catching highhresistant dust |
DE2804393C2 (en) * | 1978-02-02 | 1987-01-02 | Jens Prof. Dr. 8520 Buckenhof Christiansen | Method for generating and accelerating electrons or ions in a discharge vessel, as well as associated particle accelerator and further associated applications of the method |
KR20220027535A (en) | 2020-08-27 | 2022-03-08 | 삼성전자주식회사 | Semiconductor package and method of manufacturing the semiconductor package |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2736809A (en) * | 1945-11-06 | 1956-02-28 | Conrad G Bacon | Ion generator and projector |
US2499289A (en) * | 1947-07-02 | 1950-02-28 | John G Backus | Ion generator |
US2880337A (en) * | 1958-01-02 | 1959-03-31 | Thompson Ramo Wooldridge Inc | Particle acceleration method and apparatus |
-
1959
- 1959-10-01 US US843898A patent/US3014154A/en not_active Expired - Lifetime
-
1960
- 1960-08-19 GB GB28827/60A patent/GB916353A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1233340B (en) * | 1963-05-02 | 1967-01-26 | Csf | Electric recoil drive with an ion source |
Also Published As
Publication number | Publication date |
---|---|
US3014154A (en) | 1961-12-19 |
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