US3311772A - Focussing system for an ion source having apertured electrodes - Google Patents
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- US3311772A US3311772A US368123A US36812364A US3311772A US 3311772 A US3311772 A US 3311772A US 368123 A US368123 A US 368123A US 36812364 A US36812364 A US 36812364A US 3311772 A US3311772 A US 3311772A
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- 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
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- the present invention relates in general to an improvement in ion sources and more particularly relates to an improved electrode system for ion sources.
- a major ion optics problem in gas-discharge ion sources is the non-uniformity of the plasma density across the diameter of the source. If the electrode potentials are adjusted for good focusing from apertures near the center of the source, the arrival rate of ions at the plasma sheaths of the apertures near the periphery of the source will be too low and sheath shapes leading to poor focusing will result.
- the abovesaid problem of focusing ions from a plasma whose density has a non-uniform distribution in the sourse has been substantially resolved by means of a new type of electrode system based on a varied geometry concept. More particularly, given the radial plasma distribution of a source, the ion optics can be improved by varying the size of the apertures and. gaps of the electrode geometry in such a manner as to provide a perveance per unit area which changes radially in the same way as the ion density in the source. By so doing, substantially the same focusing conditions are then provided at the periphery of the source as at the center for the radially decreasing plasma densities encountered.
- the apertures may take the form of circular or pearshaped holes or may even have a slit configuration, or any other configuration for that matter, the only basic requirement here being that the apertures open wider, that is to say, increase in size with the radius.
- the gap or spacing between the screen and accelerating electrodes the gap or spacing is varied in the manner desired by providing the electrodes with an appropriate curvature that is related to the ion density distribution in the plasma.
- FIGURE 1 is a schematic diagram that generally illustrates an electron bombardment ion source
- FIGURES 2(a)2(e) are a series of figures that respectively illustrate the different plasma meniscus and focusing properties that may be encountered;
- FIGURES 3(a) and 3(5) are respectively front and. side views of a distributed geometry electrode system according to the present invention.
- FIGURES 4(a)4(c) present examples of alternative aperture geometries that may be used in an electrode system according to the present invention.
- FIG. 1 wherein is shown an ion source in which an electrode system according to the present invention may be utilized.
- the ion source basically includes a cylindrical arc chamber 19 with a cylindrical anode 11 supported within it.
- the anode is operated at a potential that is positive with respect to the end plates which are at cathode potential.
- One of the end plates, designated 12, is the anticathode or screen electrode and has apertures 13 through it.
- Magnet coils 14 set up a magnetic field parallel to the axis of the chamber.
- the whole chamber is run at a high positive potential V+ and an accelerating electrode 15 is run at a negative potential, the accelerating electrode having apertures 16 through it that match the apertures in the screen electrode Ions diffusing to the plasma sheath at the screen electrode can be accelerated and focused into beams by the fields across the accelerating gap 17 and through the apertures. These beams are then neutralized by the injection of electrons from an emitter at, or close to, ground potential. Under these conditions the exhaust becomes a plasma at a potential close to ground.
- the negative potential on accelerating electrode 15 provides the barrier necessary to prevent the neutralizing electrons from going back into the source. Ions are accelerated through a voltage drop of V+ plus V and decelerated through a potential V- to a velocity corresponding to the energy eV+.
- ions move toward the boundary of the plasma as a result of density and potential gradients, the number actually reaching the boundary being approximately proportional to the area of this plasma boundary surface or meniscus 18. This area varies by a factor of 2 over the extremes of a planar to a hemispherical meniscus stretched across the same aperture.
- the requirement that the field be continuous across the boundary between the plasma and accelerating region dictates that the field at the source side of screen electrode 12 be very close to 0. If the ion energies in the plasma are small compared to the energy to which they will be accelerated, the situation is similar to that of a space-charge limited ion current from a surface whose shape matches the sheath boundary.
- the surface of the plasma moves away from accelerating electrode 15 and changes the ion trajectories as well as the total ion current.
- the position of plasma meniscus 18 is, therefore, one of the most important elements of the electrode geometry. It is not a fixed surface but, rather, its position is dependent, among other things, upon the plasma, the plasma density and the accelerating voltages. Because of the plasma density dis- Q tribution at the screen electrode, the beam intensity is not uniform over the entire source area and, therefore, optimum meniscus positioning has been extremely difficult to achieve and this, as was previously mentioned, has in turn led to poor focusing.
- FIGS. 2(a)-2(e) Examples of several different kinds of beam focusing that are usually encountered with present-day electrode systems, as, for example, the electrode system shown in FIG. 1, are presented in FIGS. 2(a)-2(e), wherein the letter It stands for the ion density at any point in the plasma, that is to say, the number of ions per unit of volume in the plasma, and wherein n represents the normal or what is considered the optimum level of ion density as it was defined above. Where it is greater than n then in that kind of situation meniscus 18 moves closer to gap 17. On the other hand, where n is less than n then the meniscus is found to move away from the gap. Proper positioning of the meniscus is obtained, therefore proper beam focusing is also obtained, where 11:11 Thus FIG.
- FIGS. 2(b) 2(a) illustrates the case where n n namely, the case in which proper beam focusing is obtained.
- FIGS. 2(b) 2(a) are illustrative of poor focusing situations, namely, where n is either greater than or very much greater than n or else less than or very much less than 11
- n is either greater than or very much greater than n or else less than or very much less than 11
- this surface moves closer to the accelerating electrode which decreases the concave sheath area and slightly decreases the ion arrival rate. It can also be seen from the figures that for higher ion generation rates, the meniscus will actually become convex and produce a divergent beam with serious electrode in terception.
- FIGS. 3(a) and 3(b) An electrode system which, in accordance with the present invention, has a distributed geometry for the purpose of producing proper beam focusing across the entire ion source is illustrated in FIGS. 3(a) and 3(b).
- a view of the face of screen electrode 12 is presented in FIG. 3(a) and, as shown therein, the size of apertures 13 .is scaled with the apertures 0f smallest diameter being located at the center of the electrode and the apertures having the largest diameter being located along and following the periphery of the electrode, Between the two extremes, the apertures are graduated in size, as shown in the figures.
- FIG. 3(a) A side view of screen and accelerating electrodes 12 and 15, respectively, showing them mounted in face-to-face relationship is illustrated in FIG. 3(1)). It can be seen from this figure that the two electrodes are saucer-shaped with the convex surfaces thereof facing each other. As a result, gap 17, like the electrode apertures, is non-uniform with the spacing between the electrodes increasing with distance from their axis.
- the electrodes are spaced closer together near their centers than they are near their peripheries.
- a perveance per unit area is provided which changes radially in the same way as the ion density in the source, thereby producing good beam focusing of the type shown in FIG. 2(a).
- FIGS. 4(a)4(c) are circular in shape, it will be recognized by those skilled in the arts that the electrode geometry is not limited in this manner but, rather, that it may have other aperture configurations with equally good if not better effect. Accordingly, by way of example, several other types of aperture configurations are illustrated in FIGS. 4(a)4(c). In
- FIG. 4(a) the apertures are shown to be a plurality of pear-shaped openings with the wider part of each opening being more distant from the electrode axis than the narrower portion.
- the opening is shown to have the shape of an isosceles triangle, with the apex of the triangle at the electrode axis and the base of the tri-' angle at the circumference of the electrode.
- the apertures are shown to be in the form of slits that follow an arc of a circle and that become progressively longer as their radius of curvature increases.
- An electrode system for an ion source in which the plasma density is non-uniform across the diameter of said source comprising: screen and accelerating electrodes positioned in face-to-face relationship, said electrodes having apertures therethrough that are in registration with each other, said apertures varying in size in accordance with the radial displacement thereof from the center of the electrode and inversely as the plasma density.
- An electrode system for an ion source in which. the plasma density is non-uniform across the diameter of said source, said electrode system comprising: screen and accelerating electrodes positioned in face-to-face relationship in such a manner that the spacing therebetween varies inversely as the plasma density, said electrodes having apertures therethrough that respectively are in registration with each other and whose sizes vary in accordance with the radial displacement thereof from the center of the electrode and inversely as the plasma density.
- electrodes are saucer-shaped with the convex surfaces thereof being face-to-face, and wherein said apertures are slits that extend in a peripheral direction around the electrodes.
- An electrode system for an ion source in which the plasma density decreases with distance from the source axis comprising: a pair of saucershaped metal plates positioned with their convex surfaces in face-to-face relationship, said plates having substantially registering apertures therethrough whose size corresponds with their distance from the centers thereof; and means for applying a voltage between said plates to focus the ion beams passing therethrough.
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Description
R. c. SPEISER E L FOCUSSING SYSTEM FOR AN ION SOURCE HAVING APERTURED ELECTRODES Filed May 18 1964 March 28, 1967 INVENTOR. C. SI E/5E1? o/v 50/11.
P05527- (50/20 BY GM 3.
A 77"O/2/VEY United States Patent 3,311,772 FOCUSSING SYSTEM F01 AN ION SOURQE HAVING APERTURED ELECTRODES Robert C. Speiser, Altadena, and Gordon Sold, Pasadena,
Calif., assignors, by mesne assignments, to the United States of America as represented by the National Aeronauti-cs and Space Administration Filed May 18, 1964, Ser. No. 363,123 6 Claims. (Cl. 313-63) The invention described herein was made in the performance of work under a NASA contract and is subject to the provisions of section 305 of the National Aeronautics and Space Act of 1958, Public Law 85568 (72 Stat. 435; 42 U.S.C. 2457).
The present invention relates in general to an improvement in ion sources and more particularly relates to an improved electrode system for ion sources.
A major ion optics problem in gas-discharge ion sources is the non-uniformity of the plasma density across the diameter of the source. If the electrode potentials are adjusted for good focusing from apertures near the center of the source, the arrival rate of ions at the plasma sheaths of the apertures near the periphery of the source will be too low and sheath shapes leading to poor focusing will result.
Accordingly, it is an object of the present invention to provide a more effective ion source through the proper focusing of the ion beams.
It is another object of the present invention to rovide an electrode system that will properly focus the ion beams emitted from an ion source notwithstanding the non-uniformity of the plasma density across the diameter of the source.
The abovesaid problem of focusing ions from a plasma whose density has a non-uniform distribution in the sourse has been substantially resolved by means of a new type of electrode system based on a varied geometry concept. More particularly, given the radial plasma distribution of a source, the ion optics can be improved by varying the size of the apertures and. gaps of the electrode geometry in such a manner as to provide a perveance per unit area which changes radially in the same way as the ion density in the source. By so doing, substantially the same focusing conditions are then provided at the periphery of the source as at the center for the radially decreasing plasma densities encountered.
The apertures may take the form of circular or pearshaped holes or may even have a slit configuration, or any other configuration for that matter, the only basic requirement here being that the apertures open wider, that is to say, increase in size with the radius. As to the gap or spacing between the screen and accelerating electrodes, the gap or spacing is varied in the manner desired by providing the electrodes with an appropriate curvature that is related to the ion density distribution in the plasma.
The novel features which are believed to be characteristic of the invention, both as to its organization and method of operation, together with further objects and advantages thereof, will be better understood from the following description considered in connection with the accompanying drawing in which an embodiment of the invention is illustrated by way of example. It is to be expressly understood, however, that the drawing is for the purpose of illustration and description only and is not intended as a definition of the limits of the invention.
FIGURE 1 is a schematic diagram that generally illustrates an electron bombardment ion source;
FIGURES 2(a)2(e) are a series of figures that respectively illustrate the different plasma meniscus and focusing properties that may be encountered;
3,3 l 1,772 Patented Mar. 28, 1957 FIGURES 3(a) and 3(5) are respectively front and. side views of a distributed geometry electrode system according to the present invention; and
FIGURES 4(a)4(c) present examples of alternative aperture geometries that may be used in an electrode system according to the present invention.
Considering now the several figures in the drawing wherein like or similar parts or elements have been similarly designated, reference is made first to FIG. 1 wherein is shown an ion source in which an electrode system according to the present invention may be utilized. As depicted, the ion source basically includes a cylindrical arc chamber 19 with a cylindrical anode 11 supported within it. The anode is operated at a potential that is positive with respect to the end plates which are at cathode potential. One of the end plates, designated 12, is the anticathode or screen electrode and has apertures 13 through it. Magnet coils 14 set up a magnetic field parallel to the axis of the chamber. The whole chamber is run at a high positive potential V+ and an accelerating electrode 15 is run at a negative potential, the accelerating electrode having apertures 16 through it that match the apertures in the screen electrode Ions diffusing to the plasma sheath at the screen electrode can be accelerated and focused into beams by the fields across the accelerating gap 17 and through the apertures. These beams are then neutralized by the injection of electrons from an emitter at, or close to, ground potential. Under these conditions the exhaust becomes a plasma at a potential close to ground.
The negative potential on accelerating electrode 15 provides the barrier necessary to prevent the neutralizing electrons from going back into the source. Ions are accelerated through a voltage drop of V+ plus V and decelerated through a potential V- to a velocity corresponding to the energy eV+.
it will be noted from the figure that in the typical ion source electrode system, the spacing 17 between the screen and accelerating electrodes is a constant. It will further be noted from the figure that apertures 13 and 16, aside from being in registration with each other, are of constant size or diameter. As a result of these conditions and the fact that the plasma density is non-uniform across the diameter of the ion source, improper beam focusing is generally experienced as heretofore mentioned and as is illustrated in FIGS. 2(a)-2(e) to which reference is now made.
Generally speaking, during the process of beamformation from the plasma, ions move toward the boundary of the plasma as a result of density and potential gradients, the number actually reaching the boundary being approximately proportional to the area of this plasma boundary surface or meniscus 18. This area varies by a factor of 2 over the extremes of a planar to a hemispherical meniscus stretched across the same aperture. Moreover, the requirement that the field be continuous across the boundary between the plasma and accelerating region dictates that the field at the source side of screen electrode 12 be very close to 0. If the ion energies in the plasma are small compared to the energy to which they will be accelerated, the situation is similar to that of a space-charge limited ion current from a surface whose shape matches the sheath boundary. If the ion generation rate decreases or the gap voltage in creases, the surface of the plasma moves away from accelerating electrode 15 and changes the ion trajectories as well as the total ion current. The position of plasma meniscus 18 is, therefore, one of the most important elements of the electrode geometry. It is not a fixed surface but, rather, its position is dependent, among other things, upon the plasma, the plasma density and the accelerating voltages. Because of the plasma density dis- Q tribution at the screen electrode, the beam intensity is not uniform over the entire source area and, therefore, optimum meniscus positioning has been extremely difficult to achieve and this, as was previously mentioned, has in turn led to poor focusing.
Examples of several different kinds of beam focusing that are usually encountered with present-day electrode systems, as, for example, the electrode system shown in FIG. 1, are presented in FIGS. 2(a)-2(e), wherein the letter It stands for the ion density at any point in the plasma, that is to say, the number of ions per unit of volume in the plasma, and wherein n represents the normal or what is considered the optimum level of ion density as it was defined above. Where it is greater than n then in that kind of situation meniscus 18 moves closer to gap 17. On the other hand, where n is less than n then the meniscus is found to move away from the gap. Proper positioning of the meniscus is obtained, therefore proper beam focusing is also obtained, where 11:11 Thus FIG. 2(a) illustrates the case where n n namely, the case in which proper beam focusing is obtained. FIGS. 2(b) 2(a), on the other hand, are illustrative of poor focusing situations, namely, where n is either greater than or very much greater than n or else less than or very much less than 11 As previously indicated, if too many ions are approaching the plasma sheath, this surface moves closer to the accelerating electrode which decreases the concave sheath area and slightly decreases the ion arrival rate. It can also be seen from the figures that for higher ion generation rates, the meniscus will actually become convex and produce a divergent beam with serious electrode in terception.
An electrode system which, in accordance with the present invention, has a distributed geometry for the purpose of producing proper beam focusing across the entire ion source is illustrated in FIGS. 3(a) and 3(b). A view of the face of screen electrode 12 is presented in FIG. 3(a) and, as shown therein, the size of apertures 13 .is scaled with the apertures 0f smallest diameter being located at the center of the electrode and the apertures having the largest diameter being located along and following the periphery of the electrode, Between the two extremes, the apertures are graduated in size, as shown in the figures. In view of the fact that the apertures through the screen electrode and the apertures through the acceler ating electrode, namely, apertures 13 and 16, are in registration with each other, it will be recognized that the appearance of the two electrodes are substantially the same, or, stated differently, the frontal view in FIG. 3(a) is applicable to both electrodes. A side view of screen and accelerating electrodes 12 and 15, respectively, showing them mounted in face-to-face relationship is illustrated in FIG. 3(1)). It can be seen from this figure that the two electrodes are saucer-shaped with the convex surfaces thereof facing each other. As a result, gap 17, like the electrode apertures, is non-uniform with the spacing between the electrodes increasing with distance from their axis. In other words, the electrodes are spaced closer together near their centers than they are near their peripheries. As was indicated earlier, by thusly varying the size of the apertures and of the gap, a perveance per unit area is provided which changes radially in the same way as the ion density in the source, thereby producing good beam focusing of the type shown in FIG. 2(a).
Although the apertures through the electrodes of FIG. 3 are circular in shape, it will be recognized by those skilled in the arts that the electrode geometry is not limited in this manner but, rather, that it may have other aperture configurations with equally good if not better effect. Accordingly, by way of example, several other types of aperture configurations are illustrated in FIGS. 4(a)4(c). In
FIG. 4(a), the apertures are shown to be a plurality of pear-shaped openings with the wider part of each opening being more distant from the electrode axis than the narrower portion. In FIG. 4(b), the opening is shown to have the shape of an isosceles triangle, with the apex of the triangle at the electrode axis and the base of the tri-' angle at the circumference of the electrode. Finally, in FIG. 4(c), the apertures are shown to be in the form of slits that follow an arc of a circle and that become progressively longer as their radius of curvature increases. These are but a few examples and, therefore, still other aperture configurations may be utilized according to need.
Although a particular arrangement of the invention has been illustrated above by way of example, it is not intended that the invention be limited thereto. Accordingly, the invention should be considered to include any and all modifications, alterations, or equivalent arrangements falling within the scope of the annexed claims.
Having thus described the invention, what is claimed is:
1. An electrode system for an ion source in which the plasma density is non-uniform across the diameter of said source, said electrode system comprising: screen and accelerating electrodes positioned in face-to-face relationship, said electrodes having apertures therethrough that are in registration with each other, said apertures varying in size in accordance with the radial displacement thereof from the center of the electrode and inversely as the plasma density.
2. An electrode system for an ion source in which. the plasma density is non-uniform across the diameter of said source, said electrode system comprising: screen and accelerating electrodes positioned in face-to-face relationship in such a manner that the spacing therebetween varies inversely as the plasma density, said electrodes having apertures therethrough that respectively are in registration with each other and whose sizes vary in accordance with the radial displacement thereof from the center of the electrode and inversely as the plasma density.
3. The electrode system defined in claim 2 wherein said electrodes are saucer-shaped with the convex surfaces thereof being face-to-face, and wherein said apertures are circular, the diameters thereof changing inversely as the plasma density.
4. The electrode system defined in claim 2 wherein said electrodes are saucer-shaped with the convex surfaces thereof being face-to-face, and wherein said apertures are pear-shaped.
5. The electrode system defined in claim 2 wherein said electrodes are saucer-shaped with the convex surfaces thereof being face-to-face, and wherein said apertures are slits that extend in a peripheral direction around the electrodes.
6. An electrode system for an ion source in which the plasma density decreases with distance from the source axis, said electrode system comprising: a pair of saucershaped metal plates positioned with their convex surfaces in face-to-face relationship, said plates having substantially registering apertures therethrough whose size corresponds with their distance from the centers thereof; and means for applying a voltage between said plates to focus the ion beams passing therethrough.
References Cited by the Examiner UNITED STATES PATENTS 3,182,219 5/1965 Thomas 31361 3,213,277 10/1965 Hoppe 250-49.5(3) 3,238,715 3/1966 Reader 313-63 JAMES W. LAWRENCE, Primary Examiner.
S. SCI-ILOSSER, Assistant Examiner.
Claims (1)
- 2. AN ELECTRODE SYSTEM FOR AN ION SOURCE IN WHICH THE PLASMA DENSITY IS NON-UNIFORM ACROSS THE DIAMETER OF SAID SOURCE, SAID ELECTRODE SYSTEM COMPRISING: SCREEN AND ACCELERATING ELECTRODES POSITIONED IN FACE-TO-FACE RELATIONSHIP IN SUCH A MANNER THAT THE SPACING THEREBETWEEN VARIES INVERSELY AS THE PLASMA DENSITY, SAID ELECTRODES HAVING APERTURES THERETHROUGH THAT RESPECTIVELY ARE IN REGISTRATION WITH EACH OTHER AND WHOSE SIZES VARY IN ACCORDANCE WITH THE RADIAL DISPLACEMENT THEREOF FROM THE CENTER OF THE ELECTRODE AND INVERSELY AS THE PLASMA DENSITY.
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US368123A US3311772A (en) | 1964-05-18 | 1964-05-18 | Focussing system for an ion source having apertured electrodes |
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US368123A US3311772A (en) | 1964-05-18 | 1964-05-18 | Focussing system for an ion source having apertured electrodes |
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Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3676672A (en) * | 1969-02-03 | 1972-07-11 | Benjamin B Meckel | Large diameter ion beam apparatus with an apertured plate electrode to maintain uniform flux density across the beam |
US4028579A (en) * | 1974-10-21 | 1977-06-07 | Hughes Aircraft Company | High current density ion source |
US4684848A (en) * | 1983-09-26 | 1987-08-04 | Kaufman & Robinson, Inc. | Broad-beam electron source |
US5924277A (en) * | 1996-12-17 | 1999-07-20 | Hughes Electronics Corporation | Ion thruster with long-lifetime ion-optics system |
EP1220272A1 (en) * | 1999-07-14 | 2002-07-03 | Ebara Corporation | Beam source |
US20050257515A1 (en) * | 2004-05-18 | 2005-11-24 | The Boeing Company | A method of ionizing a liquid propellant and an electric thruster implementing such a method |
US20070033920A1 (en) * | 2005-08-11 | 2007-02-15 | The Boeing Company | Method of ionizing a liquid and an electrostatic colloid thruster implementing such a method |
US7827779B1 (en) * | 2007-09-10 | 2010-11-09 | Alameda Applied Sciences Corp. | Liquid metal ion thruster array |
US20110163674A1 (en) * | 2010-01-05 | 2011-07-07 | Kaufman & Robinson, Inc. | Mitigation of plasma-inductor termination |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3182219A (en) * | 1960-11-21 | 1965-05-04 | Gen Dynamies Corp | Mechanically modulated neutron ion chamber |
US3213277A (en) * | 1961-07-15 | 1965-10-19 | Siemens Ag | Apertured correcting diaphragm to reduce astigmatism in electron lens system |
US3238715A (en) * | 1963-09-27 | 1966-03-08 | Paul D Reader | Electrostatic ion engine having a permanent magnetic circuit |
-
1964
- 1964-05-18 US US368123A patent/US3311772A/en not_active Expired - Lifetime
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3182219A (en) * | 1960-11-21 | 1965-05-04 | Gen Dynamies Corp | Mechanically modulated neutron ion chamber |
US3213277A (en) * | 1961-07-15 | 1965-10-19 | Siemens Ag | Apertured correcting diaphragm to reduce astigmatism in electron lens system |
US3238715A (en) * | 1963-09-27 | 1966-03-08 | Paul D Reader | Electrostatic ion engine having a permanent magnetic circuit |
Cited By (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3676672A (en) * | 1969-02-03 | 1972-07-11 | Benjamin B Meckel | Large diameter ion beam apparatus with an apertured plate electrode to maintain uniform flux density across the beam |
US4028579A (en) * | 1974-10-21 | 1977-06-07 | Hughes Aircraft Company | High current density ion source |
US4684848A (en) * | 1983-09-26 | 1987-08-04 | Kaufman & Robinson, Inc. | Broad-beam electron source |
US5924277A (en) * | 1996-12-17 | 1999-07-20 | Hughes Electronics Corporation | Ion thruster with long-lifetime ion-optics system |
EP1220272A1 (en) * | 1999-07-14 | 2002-07-03 | Ebara Corporation | Beam source |
EP1220272A4 (en) * | 1999-07-14 | 2007-04-11 | Ebara Corp | Beam source |
US6996972B2 (en) * | 2004-05-18 | 2006-02-14 | The Boeing Company | Method of ionizing a liquid propellant and an electric thruster implementing such a method |
US20050257515A1 (en) * | 2004-05-18 | 2005-11-24 | The Boeing Company | A method of ionizing a liquid propellant and an electric thruster implementing such a method |
US20070033920A1 (en) * | 2005-08-11 | 2007-02-15 | The Boeing Company | Method of ionizing a liquid and an electrostatic colloid thruster implementing such a method |
US20110007446A1 (en) * | 2005-08-11 | 2011-01-13 | The Boeing Company | Electrostatic colloid thruster |
US7872848B2 (en) | 2005-08-11 | 2011-01-18 | The Boeing Company | Method of ionizing a liquid and an electrostatic colloid thruster implementing such a method |
US8122701B2 (en) | 2005-08-11 | 2012-02-28 | The Boeing Company | Electrostatic colloid thruster |
US7827779B1 (en) * | 2007-09-10 | 2010-11-09 | Alameda Applied Sciences Corp. | Liquid metal ion thruster array |
US20110163674A1 (en) * | 2010-01-05 | 2011-07-07 | Kaufman & Robinson, Inc. | Mitigation of plasma-inductor termination |
US8698401B2 (en) | 2010-01-05 | 2014-04-15 | Kaufman & Robinson, Inc. | Mitigation of plasma-inductor termination |
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