US2883568A - Apparatus for producing thermallycool charged particles - Google Patents

Apparatus for producing thermallycool charged particles Download PDF

Info

Publication number
US2883568A
US2883568A US667920A US66792057A US2883568A US 2883568 A US2883568 A US 2883568A US 667920 A US667920 A US 667920A US 66792057 A US66792057 A US 66792057A US 2883568 A US2883568 A US 2883568A
Authority
US
United States
Prior art keywords
electrons
ions
temperature
gas
electron
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 - Lifetime
Application number
US667920A
Inventor
Walter R Beam
Ronald C Knechtli
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.)
RCA Corp
Original Assignee
RCA Corp
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 RCA Corp filed Critical RCA Corp
Priority to US667920A priority Critical patent/US2883568A/en
Application granted granted Critical
Publication of US2883568A publication Critical patent/US2883568A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01JELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
    • H01J23/00Details of transit-time tubes of the types covered by group H01J25/00
    • H01J23/02Electrodes; Magnetic control means; Screens
    • H01J23/06Electron or ion guns

Definitions

  • the present invention relates to apparatus for reducing the temperature of charged particles, and especially to apparatus for producing an ultra low noise low temperature electron beam in high vacuum.
  • the electro-n stream may be said to possess -a temperature. This temperature is substantially equal to the temperature of the emitter.
  • the factors determining the noise gure (a measure of the noise introduced by the device) of a microwave beam amplifier device, such as a traveling-wave tube, are mainly the current and velocity fluctuations in the beam. The current fluctuations are independent of the temperature. However, the mean square value of the velocity fluctuations is proportional to the emitter temperature.
  • a stream of electrons is cooled by means of thermalizing nonionizing collisions of the electrons with the molecules f a cool gas, such as ammonia or hydrogen, in the presence of sutlcient positive ions to neutralize the space charge ⁇ of the electrons and thereby permit the production of substantial beam currents at low electron drift velocities.
  • the temperature of the cooling gas may be of the order of room temperature, or less.
  • the pressure of the gas in the cooling region may be between 5 and 101 mm. of Hg, and is preferably about l03 mm., or lp. of Hg.
  • evacuating means are provided for progressively reducing the pressure of the cooling gas along the stream.
  • a magnetic field axial to the stream is provided to conine the electrons and ions to the stream throughout the cooling and evacuating regions.
  • Means are provided at the output end for extracting the cool electrons from the 'stream and accelerating them uniformly along a desired path.
  • the positive ions can be produced independently of the electrons to be cooled, for example at the other end of the apparatus.
  • the electrons are produced by bombardment heating a tungsten plate to electron emitting temperature, and the ions 'are produced by contact ionization of atoms of an alkaline metal vapor, such as cesium, at the hot surface of the tungsten plate.
  • the electrons and ions thus produced are caused to drift slowly, in the same general direction, through a cooling region containing the cooling gas and la pumping region to the output end of the apparatus Where the cooled electrons are separated from the positive ions and formed into a cool ultra low noise, high-vacuum beam.
  • the low temperature electron beam produced by the invention can be used for any electron tube requiring appreciable electron current with low velocity spread, such as ultra low noise microwave tubes, or for basic physical research.
  • An object of the invention is to provide means for reducing the temperature of charged particles.
  • Another object of the invention is to provide means for producing a low temperature plasma stream.
  • a further object of the invention is to provide means for producing a low temperature, low noise electron beam in high vacuum.
  • Still another object is -to provide a new and improved source of a plasma made up of electrons and positive ions.
  • Fig. l is a side View, partly in axial section, of one embodiment of apparatus for producing 'a low temperature beam of electrons in high vacuum according to the present invention
  • Fig. 2 is a schematic view similar to Fig. l of another embodiment of the invention.
  • Fig. 3 is an axial sectional view of the plasma emitter and gas inlet assembly of Fig. 2.
  • the invention provides means for greatly reducing the thermal velocities of electrons emitted from a thermionic source by mixfing them With a cooler gas.
  • a thermionic cathode operated near room temperature but capable of delivering enough current to operate low-noise microwave ampliers and similar devices.
  • the noise iigure of beam type ampliers clan theoretically be reduced to 3 decibels or less.
  • Conventional low noise microwave amplijers without electron cooling have noise figures of about 5 decibels, at best, and more commonly about 7 decibels.
  • the sizable beam currents needed for microwave ⁇ devices require ion neutralization if the elec- 'trons are to pass through the cooling region at slow enough speed to be ⁇ cooled to nearly the temperature of the gas, which may be room temperature, or less.
  • the neutralizing ions should not contribute an appreciable amount of energy to the system, and must not recombine ⁇ at an excessive rate with the electrons or with the cooling gas.
  • the cooling gas since the cooling gas must be present at a moderate pressure it is necessary to evacuate the gas from the plasma stream after cooling in order to obtain a good vacuum in the output region.
  • the electrons are most conveniently produced by means of a thermionic emitter.
  • An attractive means of positive ion lsupply is the phenomenon of contact ionization. If a metal surface is heated in the presence of atoms having an ionization potential less than the work function of the metal, atoms which impinge on the metal surface Will be ionized by the ailinity of the surface for their electrons. The heat of the surface will then drive oit lthe ions, resulting in a source of positive ions having a temperature substantially equal to the emitter temperature.
  • the atoms of cesium, potassium and rubidium satisfy the condition for contact ionization. lf the tungsten is heated to electron emitting temperature the surface becomes a source of both positive ions and electrons, or a plasma emitter.
  • the gas is removed from the plasma stream after cooling by means of a plurale-age vacuum ing arrangement in which several pumps reduce the gas pressure through a series of constrictions.
  • a plurale-age vacuum ing arrangement in which several pumps reduce the gas pressure through a series of constrictions.
  • the electrons must pass from the emitter through the cooling and pumping regions to the high vacuum region.
  • the positive ions must be present to substantially neutralize the space charge, between the electron emitter and the region where the electrons are accelerated to high velocity, one has a choice as to the direction of the ions.
  • the ions may originate with the electrons and travel through the apparatus in the same direction. Alternatively, the ions may originate at a separate ion source at the opposite end of the apparatus, in which case the ions and electrons travel in opposite directions,
  • the electrons are drawn through the gas by a weak axial electric field set up by a low positive potential on an electron extractor electrode in the high vacuum region.
  • the ions are carried through the cooling and pumping regions by the ilow of the co-oling gas itself.
  • a separate chemically-inactive gas7 such as nitrogen or argon, for example, may be passed through the apparatus, in addition to the cooling gas, for transporting the ions.
  • an inactive gas can be used to prevent excessive quantities of the cooling gas from reaching the emitter. Both of these functions can be performed by the same inactive gas.
  • Transverse constraint of the plasma will prevent loss of any appreciable number of electrons or ions to the surrounding walls.
  • This constraint may be obtained by the provision of a strong axial magnetic ield extending along the length of the plasma stream. This lield limits the electrons to movement in tight circles in a transverse plane, which means that the greatest distance by which they can move outward, per collision, is the diameter of this circular path.
  • the field is made strong enough that this diameter is several orders of magnitude smaller than the stream diameter, so that the electrons cannot move transversely to any appreciable extent in the length of the cooling region.
  • ions because of their much greater mass, are not so constrained but, if a number of ions leave the region containing the electrons, the potential on the axis is depressed and a natural ion trap is formed. ln order to prevent excessive depression of the plasma. stream potential, an alternative consists in raising the potentials on the Walls surrounding the stream by a small fraction of a volt.
  • the electrons must he separated from the ions at the high vacuum end of the apparatus. This may be accomplished by means of a cylindrical ion-collecting electrode, closely surround ing the plasma stream, at approximately the potential of the edge of the stream or slightly negative with respect thereto, followed by the electron accelerating electrode. As the number of ions in the stream is reduced, there would normally be a drop in stream potential. However, this drop will be approximately compensated by the accelerating electrode, and the electrons will be accelerated to high velocities only in the region beyond the ioncollecting electrode.
  • Fig. l shows, for example, an embodiment of the invention comprising an elongated tubular enclosure l, which may be of glass, having a cooling gas inlet tubing 3 at the left end, a plurality of exhaust holes 5 spaced along the side thereof and an output tubing 7 at the right end adapted to be vacuum-sealed to a device for utilizing the low temperature electron beam produced within the enclosure l.
  • a source 9 of electrons and positive ions is mounted within the enclosure ll near the gas. inlet tubing 3 to provide a plasma stream 1l directed toward the outlet tubing 7.
  • the source 9, schematically shown in Fig. l, is preferably of the contact ionization type shown in Fig. 2. Spaced from the source 9 is the first of three tubular constricting members l2, which form parts ⁇ of a difterential, three-stage pumping system.
  • the space between the source 9 and the tirst member 13 constitutes a cooling ychamber 14 wherein electrons and ions from the source 9 are cooled by non-ionizing collisions with the molecules of the cooling gas.
  • the cooling gas is preferably ammonia, in pure form, at room temperature and at an initial pressure of about lu of Hg.
  • the drift velocity of the electrons in the cooling region be about two orders of magnitude less than their initial mean thermal velocity, which is determined by the emitter temperature. This means a drift velocity of the order of om./sec.
  • This drift velocity corresponds to an electron velocity of less than 3 X l05 volts, which is far below the ionization potential of the gases used in the apparatus.
  • To obtain a desired current density of a few ma./cm.2 with such a low drift velocity requires electron densities of the order of 1010 to 1011 electrons/cm3, which makes it necessary to use positive ion space charge neutralization.
  • the constricting members 13 are positioned along the enclosure ll to provide pumping chambers 15 and ll7 registering With the holes 5. Each of these chambers opens into one of three high vacuum pumps 19 which are sealed by suitable means (not shown) to the enclosure ll around the holes 5.
  • the high pressure sides of the three pumps i9 may be connected together, as shown, by a gas outlet tubing 21, which may be connected to a mechanical fore pump (not shown). Alternatively, the same cooling gas may be used yover again by connecting the outlet tubing 21 directly to the inlet tubing 3.
  • the pumping system shown in Fig. 1 produces a pressure dilferential in the regions indicated in which P1 P2 P3 P4.
  • the pressure is substantially constant across each region, with a gradual pressure gradient along each of the constricting members 13.
  • the final pressure in chamber 17 should be 10-6 mm. of Hg, or less, in order to produce a high vacuum at the output end 7 of the apparatus.
  • potentials V1, V2 and V3 may be applied to the constricting members 13 such that Vlgd volt, Val volt, and VlVzT/g, as shown in Fig. l, to prevent excessive depression of the plasma stream potential.
  • the plasma stream After passing through the pumping system, the plasma stream enters an electron extraction region where the positive ions are collected by a cylindrical ion collector 23 at a potential of .1 to -10 volts, and the electrons are accelerated by an annular accelerating electrode 25 at a substantial positive potential, of the order of +50 volts, relative to the source 9.
  • An axial magnetic eld B for transversely constraining the plasma may be produced by any suitable means, such as Ione or more electromagnets coaxially surrounding the enclosure 1.
  • Fig. 2 schematically shows another apparatus, incorporating the basic principles of the present invention, including the preferred contact ionization type of plasma emitter in combination with an improved differential pumping system that is disclosed and claimed in a copending application of Ronald C. Knechtli, Serial No. 667,943, led concurrently herewith, now Patent No. 2,841,726, issued July 1, 1958.
  • the apparatus sho-wn in Fig. 2 comprises an elongated enclosure 29 containing a plasma emitter 31, a cooling chamber 33, a differential pumping system 35, an electron extractor structure 37, and a high vacuum region 39.
  • the plasma emitter and gas inlet assembly of Fig. 2 is shown in detail in Fig. 3 and comprises an inner tubular member 41, on which the plasma emitter 31 is mounted,
  • a concentric outer tubular member 43 which forms an end portion of the enclosure Z9.
  • a third tubular member 45 Concentrically mounted between the members 41 and 43 is a third tubular member 45 which separates the cooling gas from the transport gas, when the latter is used, and serves to keep the cooling Igas cool by minimizing heat transfer from the hot plasma emitter 31.
  • the plasma emitter 31 comprises a tungsten plate 47, having a thickness of about mils, transversely mounted at the right hand end of the member 41 by means of a thin apertured disc 49 of tantalum, to which the plate 47 is welded, clamped in substantially vacuum-tight relation to the end of member 41 by a ring 51.
  • a cathode 53 is positioned behind the tungsten plate 47 for heating the latter by electron bombardment.
  • the cathode 53 is Imounted in insulated relation within a tubular accelerating electrode 55. Leads 47 for the cathode and accelerating electrode extend through an insulating end closure 59 vacuum sealed to the opposite end of the member 41.
  • a cesium evaporator 61 is mounted on one side of the member 43 with a cesium supply tube 63 extending through the tubular members 43 and 45 in position to direct a stream of cesium vapor atoms through the ring 51 toward the front surface of the tungsten plate 47.
  • the cooling gas which may be ammonia or hydrogen, for example, is supplied at 65 to the annular space between the two outer tubular members 43 and 45.
  • the right hand ends of the members 43 and 45 include converging conical members 43a and 45a which provide a converging annular passage therebetween leading to the cooling chamber 33.
  • the structure shown may be used with an inactive gas, in which case the inactive gas is supplied at 67 to the space between the two inner tubular members 41 and 43 and flows past the plasma emitter 31 carrying the ions through the cooling and pumping regions'.
  • the ions will usually have suicient initial velocities due to their temperature to reach the cooling chamber 33. If the cooling gas flow can effectively transport the ions and if its dissociation products at the hot tungsen plate are ⁇ not harmful, the separate gas can be dispensed with.
  • the diiferential pumping system shown schematically in Fig. 2 comprises an elongated perforated metal tube 69 extending Within the enclosure 29 from the cooling chamber 33 to the electron extractor 37.
  • the space between the tube 69 and enclosure 29 is separated into three pumping chambers 71 by means of two annular partitions 73.
  • Each of the chambers 71 is connected to a high Vacuum pump (not shown).
  • the pumps may be connected to a mechanical fore pump or to the cooling gas inlet 65, as described in connection with Fig. 1.
  • the apertures 75 in the tube 69 may be distributed around and along the tube in either random or systematic order.
  • each pumping chamber 71 tit is preferred that the number of apertures or their size, or both, be chosen so that the total aperture area per unit axial length will increase along each pumping chamber 71 in the manner described in said copending application.
  • the pressure in each chamber 71 outside the tube 69 will be substantially uniform at a value approximately equal to the pressure inside the tube 69 at the low pressure end of the part of the tube within that chamber, wheras the pressure within the tube 69 will progressively decrease throughout its entire length.
  • the electron extractor 37 and high vacuum region 39 may be the same as ⁇ in Fig. 1.
  • Apparatus for cooling electrons comprising: a source of electrons having a mean thermal velocity determining a given initial electron temperature; a chamber containing a cooling gas having a temperature substantially lower than said initial electron temperature; means independent of said cooling gas for providing positive ions in said chamber; land means for causing said electrons to drift through said chamber at a drift velocity substantially less than said mean thermal velocity, whereby said electrons are cooled to a temperature substantially lower than said initial electron temperature as a result of non-ionizing collisions with the molecules of said gas.
  • Apparatus for producing a low temperature plasma stream comprising: a common source of electrons and positive ions, said electrons having a mean thermal velocity determining an initial electron temperature substantially higher than room temperature; a chamber containing a cooling gas having a temperature substantially lower than said initial electron temperature; and means for causing said electrons and ions to drift through said chamber in the same general direction at velocities substantially less than said mean thermal electron velocity, whereby said electrons are cooled to a temperature substantially below said initial electron temperature as a result of non-ionizing collisions with the molecules of said cooling gas.
  • Apparatus according to claim 2 wherein said source of electrons and positive ions comprises a member having an electron emissive surface with a given work function, means for heating said member to electron emitting temperature, and means for supplying metal vapor atoms at said surface of said member for contact ionization thereat having an ionization potential less than said work function.
  • Apparatus for producing a low temperature plasma stream comprising: a first chamber and means for supplying a gas thereto having a temperature no higher than room temperature and an initial pressure between l0-5 and 10-1 mm. of Hg; means for supplying a stream of electrons and positive ions to said chamber, said electrons having a mean thermal velocity determining an initial electron temperature substantially higher than room temperature; means for causing said electrons and ions to drift through said chamber in the same general direction at a drift Velocity Substantially less than said mean thermal electron velocity, whereby said electrons and ions are cooled to a temperature substantially below said initial electron temperature as a result of collisions with the molecules of said gas; a second chamber cornmunicating with said first chamber through which said ions and electrons drift after passage through said rst chamber; means for progressively reducing the gas pressure in said second chamber in the direction ,of drift to a pressure at the end remote from said iirst chamber substantially lower than said initial pressure; and means for minimizing loss of electron
  • Apparatus according to claim 5, wherein said means for causing said ions to drift comprises said gas which by its flow through said apparatus imparts momentum to said ions.
  • Apparatus according to claim 5, wherein said means for causing said ions to drift comprises means for supplying and directing a separate inactive gas through said apparatus for imparting momentum to said ions.
  • Apparatus for producing a beam of low temperature electrons comprising: a source of electrons having a mean thermal velocity determining an initial electron temperature substantially higher than room temperature; a first chamber ⁇ and means for supplying a gas thereto having a temperature substantially lower than said initial electron temperature and an initial pressure between 10*5 and l0*1 mm.
  • Apparatus according to claim 8 wherein said means for causing said electrons to drift and said last-named means comprise an electron accelerating electrode located at said remote end of said second chamber.
  • Apparatus for producing a beam of low temperature electrons comprising: a rst chamber and means for supplying a gas thereto having a temperature no higher than room temperature and an initial pressure between 10-5 and 10-l mm. of Hg; means for supplying a stream of electrons and positive ions to said chamber, said electrons having a mean thermal velocity determining an initial electron temperature substantially higher than room temperature; means for causing said electrons and ions to drift through said chamber in the same general direction at a drift velocity substantially less than said mean thermal electron velocity, whereby said electrons and ions are cooled to a temperature substantially below said initial electron temperature as a result of collisions with the molecules of said gas; a second chamber communicating with said rst chamber through which said ions and electrons drift after passage through said irst chamber; means for progressively reducing the gas pressure in said second chamber in the direction of drift to a pressure at the end thereof remote from said rst chamber substantially lower than said initial pressure; means for producing a confining magnetic
  • a source of electrons and positive ions comprising a member metal having an electron emissive surface with a given work function, means for bombarding said member with electrons to heat said member to electron emitting temperature, land means for supplying at said surface of said member for contact ionization thereat metal vapor atoms having an ionization potential less than said work function, said atoms being provided by continuous evaporation of atoms from an alkaline metal.

Landscapes

  • Electron Sources, Ion Sources (AREA)

Description

April 2l, 1959 w. RQBEAM ETAL 2,883,568
APPARATUS FOR PRoDucING THERMALLY-coor.. CHARGED `PARTICARS Filed June 25, 1957 :La: nea/v :021 /A/a /fx fueras l g STREAM INVENTORS f5/7 5a/'ea'- 'WALTER R .BEAM AN United States Patent APPARATUS FOR PRODUCING THERMALLY- COOL CHARGED PARTICLES Walter R..Beam, Trenton, and Ronald C. Knechtli, Cranbury, NJ., assignors to Radio Corporation of America, a corporation of Delaware Application June 25, 1957, Serial No. 667,920
13 Claims. (Cl. 313-7) The present invention relates to apparatus for reducing the temperature of charged particles, and especially to apparatus for producing an ultra low noise low temperature electron beam in high vacuum.
When electrons are emitted from a thermionic emitter or cathode they leave, not at a uniform velocity, but with a thermionic velocity spread. Since such a velocity spread is typical of a heated gas, the electro-n stream may be said to possess -a temperature. This temperature is substantially equal to the temperature of the emitter. The factors determining the noise gure (a measure of the noise introduced by the device) of a microwave beam amplifier device, such as a traveling-wave tube, are mainly the current and velocity fluctuations in the beam. The current fluctuations are independent of the temperature. However, the mean square value of the velocity fluctuations is proportional to the emitter temperature. Thus, if one could nd some way to reduce the temperature of the emitter, or of the electron beam itself, a new way to reduce the noise gure of microwave ampliers would be available. Reducing the temperature of the emitter below a certain point is not possible, because of the way in which thermionic emitters operate, and because of the non-existence of emissive materials with very low work function. One method of reducing the thermal velocity spread of the electrons in a beam is that of velocity selection, e.g. utilizing magnetic deflection. ln velocity selection, only electrons within a narrow part of the Maxwellian velocity distribution are used. Also, space charge eiects defeat attempts to realize a velocity selector capable of yielding appreciable currents or current densities. Typical orders of magnitude of room teinperature electron currents obtainable with velocity selectors are of the order of 104 ampere.
In accordance with the present invention, a stream of electrons is cooled by means of thermalizing nonionizing collisions of the electrons with the molecules f a cool gas, such as ammonia or hydrogen, in the presence of sutlcient positive ions to neutralize the space charge `of the electrons and thereby permit the production of substantial beam currents at low electron drift velocities. The temperature of the cooling gas may be of the order of room temperature, or less. The pressure of the gas in the cooling region may be between 5 and 101 mm. of Hg, and is preferably about l03 mm., or lp. of Hg. In order to obtain a good vacuum in the region at the output end of the apparatus Where the cooled electrons are to be utilized, evacuating means are provided for progressively reducing the pressure of the cooling gas along the stream. A magnetic field axial to the stream is provided to conine the electrons and ions to the stream throughout the cooling and evacuating regions. Means are provided at the output end for extracting the cool electrons from the 'stream and accelerating them uniformly along a desired path.
The positive ions can be produced independently of the electrons to be cooled, for example at the other end of the apparatus. However, in the preferred embodiment of Patented Apr. 21, 1959 ICC the invention, the electrons are produced by bombardment heating a tungsten plate to electron emitting temperature, and the ions 'are produced by contact ionization of atoms of an alkaline metal vapor, such as cesium, at the hot surface of the tungsten plate. The electrons and ions thus produced are caused to drift slowly, in the same general direction, through a cooling region containing the cooling gas and la pumping region to the output end of the apparatus Where the cooled electrons are separated from the positive ions and formed into a cool ultra low noise, high-vacuum beam.
The low temperature electron beam produced by the invention can be used for any electron tube requiring appreciable electron current with low velocity spread, such as ultra low noise microwave tubes, or for basic physical research. t
An object of the invention is to provide means for reducing the temperature of charged particles.
Another object of the invention is to provide means for producing a low temperature plasma stream.
A further object of the invention is to provide means for producing a low temperature, low noise electron beam in high vacuum.
Still another object is -to provide a new and improved source of a plasma made up of electrons and positive ions.
ln the annexed drawing:
Fig. l is a side View, partly in axial section, of one embodiment of apparatus for producing 'a low temperature beam of electrons in high vacuum according to the present invention;
Fig. 2 is a schematic view similar to Fig. l of another embodiment of the invention; and
Fig. 3 is an axial sectional view of the plasma emitter and gas inlet assembly of Fig. 2.
The invention provides means for greatly reducing the thermal velocities of electrons emitted from a thermionic source by mixfing them With a cooler gas. By providing positive ions for neutralizing the space charge of the electrons, transporting the electrons and ions, pumping away the cooling gas and nally extracting the cool electrons from the plasma, the resulting electron stream is the equivalent of a thermionic cathode operated near room temperature but capable of delivering enough current to operate low-noise microwave ampliers and similar devices. By this means the noise iigure of beam type ampliers clan theoretically be reduced to 3 decibels or less. Conventional low noise microwave amplijers without electron cooling have noise figures of about 5 decibels, at best, and more commonly about 7 decibels.
In -order to carry ourt the desired cooling of the electrons and end up with a substantial beam current in a region of high vacuum, there are certain basic requirements. First, the sizable beam currents needed for microwave `devices require ion neutralization if the elec- 'trons are to pass through the cooling region at slow enough speed to be `cooled to nearly the temperature of the gas, which may be room temperature, or less. The neutralizing ions should not contribute an appreciable amount of energy to the system, and must not recombine `at an excessive rate with the electrons or with the cooling gas. Second, since the cooling gas must be present at a moderate pressure it is necessary to evacuate the gas from the plasma stream after cooling in order to obtain a good vacuum in the output region. Third, since the electron drift velocity must be very small, and the electrons must be accelerated by appreciable voltages in Ithe region where they are used, means must be provided for carrying the electrons slowly through the cooling and pumping regions, and accelerating them when Ithey reach the high vacuum region. At the same time, the ions must be carried from their point of origin to the opposite end of the plasma stream so that they are at all times in position to neutralize the electronic space charge. Finally, provision must be made for separating the electrons from the ions in the region where the electrons are accelerated.
The electrons are most conveniently produced by means of a thermionic emitter. An attractive means of positive ion lsupply is the phenomenon of contact ionization. If a metal surface is heated in the presence of atoms having an ionization potential less than the work function of the metal, atoms which impinge on the metal surface Will be ionized by the ailinity of the surface for their electrons. The heat of the surface will then drive oit lthe ions, resulting in a source of positive ions having a temperature substantially equal to the emitter temperature. In the case of tungsten as the heated metal, the atoms of cesium, potassium and rubidium satisfy the condition for contact ionization. lf the tungsten is heated to electron emitting temperature the surface becomes a source of both positive ions and electrons, or a plasma emitter.
Preferably, the gas is removed from the plasma stream after cooling by means of a plurale-age vacuum ing arrangement in which several pumps reduce the gas pressure through a series of constrictions. This is a very eifective method because of the fact that normal diffusion pumps have constant speed (volumetric) over a wide range of pressures, which means that a plurality of pumps can reduce the pressure in approximately a geometric progression. ln cases where the low-temperature stream does not require a high vacuum, the differential pumping arrangement may be reduced to a single stage, or eliminated.
The electrons must pass from the emitter through the cooling and pumping regions to the high vacuum region. Although the positive ions must be present to substantially neutralize the space charge, between the electron emitter and the region where the electrons are accelerated to high velocity, one has a choice as to the direction of the ions. The ions may originate with the electrons and travel through the apparatus in the same direction. Alternatively, the ions may originate at a separate ion source at the opposite end of the apparatus, in which case the ions and electrons travel in opposite directions, The electrons are drawn through the gas by a weak axial electric field set up by a low positive potential on an electron extractor electrode in the high vacuum region. Where electrons and ions travel in the same direction, due to their opposite charge, the ions must be transported by some means other than the axial electric field. in the preferred practice of the invention, the ions are carried through the cooling and pumping regions by the ilow of the co-oling gas itself. If the cooling gas is incapable of transporting the ions, a separate chemically-inactive gas7 such as nitrogen or argon, for example, may be passed through the apparatus, in addition to the cooling gas, for transporting the ions. lf the cooling gas has adverse effects on the plasma emitter, an inactive gas can be used to prevent excessive quantities of the cooling gas from reaching the emitter. Both of these functions can be performed by the same inactive gas.
In order to cool electrons efficiently it is necessary to use a gas which is either very light in mass or one which has a great many molecular degrees of freedom, enabling the molecules to be spun or vibrated by collision with electrons. Examples of such gases are ammonia, carbon dioxide, pentane and benzene. However, the more complex molecules, while making very effective cooling media, are very easy to dissociate into undesirable components. Therefore, ammonia is preferred. The only light-weight molecule with satisfactory cooling properties is hydrogen, which is practically harmless even when dissociated.
Transverse constraint of the plasma will prevent loss of any appreciable number of electrons or ions to the surrounding walls. This constraint may be obtained by the provision of a strong axial magnetic ield extending along the length of the plasma stream. This lield limits the electrons to movement in tight circles in a transverse plane, which means that the greatest distance by which they can move outward, per collision, is the diameter of this circular path. The field is made strong enough that this diameter is several orders of magnitude smaller than the stream diameter, so that the electrons cannot move transversely to any appreciable extent in the length of the cooling region. The ions, because of their much greater mass, are not so constrained but, if a number of ions leave the region containing the electrons, the potential on the axis is depressed and a natural ion trap is formed. ln order to prevent excessive depression of the plasma. stream potential, an alternative consists in raising the potentials on the Walls surrounding the stream by a small fraction of a volt.
In the preferred type ot operation in which the electrous and ions drift in the same direction, the electrons must he separated from the ions at the high vacuum end of the apparatus. This may be accomplished by means of a cylindrical ion-collecting electrode, closely surround ing the plasma stream, at approximately the potential of the edge of the stream or slightly negative with respect thereto, followed by the electron accelerating electrode. As the number of ions in the stream is reduced, there would normally be a drop in stream potential. However, this drop will be approximately compensated by the accelerating electrode, and the electrons will be accelerated to high velocities only in the region beyond the ioncollecting electrode.
Fig. l shows, for example, an embodiment of the invention comprising an elongated tubular enclosure l, which may be of glass, having a cooling gas inlet tubing 3 at the left end, a plurality of exhaust holes 5 spaced along the side thereof and an output tubing 7 at the right end adapted to be vacuum-sealed to a device for utilizing the low temperature electron beam produced within the enclosure l.
A source 9 of electrons and positive ions is mounted Within the enclosure ll near the gas. inlet tubing 3 to provide a plasma stream 1l directed toward the outlet tubing 7. The source 9, schematically shown in Fig. l, is preferably of the contact ionization type shown in Fig. 2. Spaced from the source 9 is the first of three tubular constricting members l2, which form parts `of a difterential, three-stage pumping system.
The space between the source 9 and the tirst member 13 constitutes a cooling ychamber 14 wherein electrons and ions from the source 9 are cooled by non-ionizing collisions with the molecules of the cooling gas. The cooling gas is preferably ammonia, in pure form, at room temperature and at an initial pressure of about lu of Hg. In order to cool the electrons down close to the gas temperature, it is necessary that the drift velocity of the electrons in the cooling region be about two orders of magnitude less than their initial mean thermal velocity, which is determined by the emitter temperature. This means a drift velocity of the order of om./sec. This drift velocity corresponds to an electron velocity of less than 3 X l05 volts, which is far below the ionization potential of the gases used in the apparatus. To obtain a desired current density of a few ma./cm.2 with such a low drift velocity requires electron densities of the order of 1010 to 1011 electrons/cm3, which makes it necessary to use positive ion space charge neutralization.
The constricting members 13 are positioned along the enclosure ll to provide pumping chambers 15 and ll7 registering With the holes 5. Each of these chambers opens into one of three high vacuum pumps 19 which are sealed by suitable means (not shown) to the enclosure ll around the holes 5. The high pressure sides of the three pumps i9 may be connected together, as shown, by a gas outlet tubing 21, which may be connected to a mechanical fore pump (not shown). Alternatively, the same cooling gas may be used yover again by connecting the outlet tubing 21 directly to the inlet tubing 3.
The pumping system shown in Fig. 1 produces a pressure dilferential in the regions indicated in which P1 P2 P3 P4. The pressure is substantially constant across each region, with a gradual pressure gradient along each of the constricting members 13. The final pressure in chamber 17 should be 10-6 mm. of Hg, or less, in order to produce a high vacuum at the output end 7 of the apparatus.
If desired, potentials V1, V2 and V3 may be applied to the constricting members 13 such that Vlgd volt, Val volt, and VlVzT/g, as shown in Fig. l, to prevent excessive depression of the plasma stream potential.
After passing through the pumping system, the plasma stream enters an electron extraction region where the positive ions are collected by a cylindrical ion collector 23 at a potential of .1 to -10 volts, and the electrons are accelerated by an annular accelerating electrode 25 at a substantial positive potential, of the order of +50 volts, relative to the source 9.
An axial magnetic eld B for transversely constraining the plasma may be produced by any suitable means, such as Ione or more electromagnets coaxially surrounding the enclosure 1.
Fig. 2 schematically shows another apparatus, incorporating the basic principles of the present invention, including the preferred contact ionization type of plasma emitter in combination with an improved differential pumping system that is disclosed and claimed in a copending application of Ronald C. Knechtli, Serial No. 667,943, led concurrently herewith, now Patent No. 2,841,726, issued July 1, 1958. The apparatus sho-wn in Fig. 2 comprises an elongated enclosure 29 containing a plasma emitter 31, a cooling chamber 33, a differential pumping system 35, an electron extractor structure 37, and a high vacuum region 39.
The plasma emitter and gas inlet assembly of Fig. 2 is shown in detail in Fig. 3 and comprises an inner tubular member 41, on which the plasma emitter 31 is mounted,
and a concentric outer tubular member 43 which forms an end portion of the enclosure Z9. Concentrically mounted between the members 41 and 43 is a third tubular member 45 which separates the cooling gas from the transport gas, when the latter is used, and serves to keep the cooling Igas cool by minimizing heat transfer from the hot plasma emitter 31.
The plasma emitter 31 comprises a tungsten plate 47, having a thickness of about mils, transversely mounted at the right hand end of the member 41 by means of a thin apertured disc 49 of tantalum, to which the plate 47 is welded, clamped in substantially vacuum-tight relation to the end of member 41 by a ring 51. A cathode 53 is positioned behind the tungsten plate 47 for heating the latter by electron bombardment. The cathode 53 is Imounted in insulated relation within a tubular accelerating electrode 55. Leads 47 for the cathode and accelerating electrode extend through an insulating end closure 59 vacuum sealed to the opposite end of the member 41.
A cesium evaporator 61 is mounted on one side of the member 43 with a cesium supply tube 63 extending through the tubular members 43 and 45 in position to direct a stream of cesium vapor atoms through the ring 51 toward the front surface of the tungsten plate 47.
The cooling gas, which may be ammonia or hydrogen, for example, is supplied at 65 to the annular space between the two outer tubular members 43 and 45. The right hand ends of the members 43 and 45 include converging conical members 43a and 45a which provide a converging annular passage therebetween leading to the cooling chamber 33. The structure shown may be used with an inactive gas, in which case the inactive gas is supplied at 67 to the space between the two inner tubular members 41 and 43 and flows past the plasma emitter 31 carrying the ions through the cooling and pumping regions'. The ions will usually have suicient initial velocities due to their temperature to reach the cooling chamber 33. If the cooling gas flow can effectively transport the ions and if its dissociation products at the hot tungsen plate are `not harmful, the separate gas can be dispensed with.
The diiferential pumping system shown schematically in Fig. 2 comprises an elongated perforated metal tube 69 extending Within the enclosure 29 from the cooling chamber 33 to the electron extractor 37. The space between the tube 69 and enclosure 29 is separated into three pumping chambers 71 by means of two annular partitions 73. Each of the chambers 71 is connected to a high Vacuum pump (not shown). The pumps may be connected to a mechanical fore pump or to the cooling gas inlet 65, as described in connection with Fig. 1. The apertures 75 in the tube 69 may be distributed around and along the tube in either random or systematic order. However, tit is preferred that the number of apertures or their size, or both, be chosen so that the total aperture area per unit axial length will increase along each pumping chamber 71 in the manner described in said copending application. In this pumping system the pressure in each chamber 71 outside the tube 69 will be substantially uniform at a value approximately equal to the pressure inside the tube 69 at the low pressure end of the part of the tube within that chamber, wheras the pressure within the tube 69 will progressively decrease throughout its entire length.
The electron extractor 37 and high vacuum region 39 may be the same as` in Fig. 1.
What is claimed is:
l. Apparatus for cooling electrons comprising: a source of electrons having a mean thermal velocity determining a given initial electron temperature; a chamber containing a cooling gas having a temperature substantially lower than said initial electron temperature; means independent of said cooling gas for providing positive ions in said chamber; land means for causing said electrons to drift through said chamber at a drift velocity substantially less than said mean thermal velocity, whereby said electrons are cooled to a temperature substantially lower than said initial electron temperature as a result of non-ionizing collisions with the molecules of said gas.
2. Apparatus for producing a low temperature plasma stream comprising: a common source of electrons and positive ions, said electrons having a mean thermal velocity determining an initial electron temperature substantially higher than room temperature; a chamber containing a cooling gas having a temperature substantially lower than said initial electron temperature; and means for causing said electrons and ions to drift through said chamber in the same general direction at velocities substantially less than said mean thermal electron velocity, whereby said electrons are cooled to a temperature substantially below said initial electron temperature as a result of non-ionizing collisions with the molecules of said cooling gas.
3. Apparatus according to claim 2, wherein said source of electrons and positive ions comprises a member having an electron emissive surface with a given work function, means for heating said member to electron emitting temperature, and means for supplying metal vapor atoms at said surface of said member for contact ionization thereat having an ionization potential less than said work function.
4. Apparatus according to claim 3, wherein said member is tungsten, and said metal vapor is cesium.
5. Apparatus for producing a low temperature plasma stream comprising: a first chamber and means for supplying a gas thereto having a temperature no higher than room temperature and an initial pressure between l0-5 and 10-1 mm. of Hg; means for supplying a stream of electrons and positive ions to said chamber, said electrons having a mean thermal velocity determining an initial electron temperature substantially higher than room temperature; means for causing said electrons and ions to drift through said chamber in the same general direction at a drift Velocity Substantially less than said mean thermal electron velocity, whereby said electrons and ions are cooled to a temperature substantially below said initial electron temperature as a result of collisions with the molecules of said gas; a second chamber cornmunicating with said first chamber through which said ions and electrons drift after passage through said rst chamber; means for progressively reducing the gas pressure in said second chamber in the direction ,of drift to a pressure at the end remote from said iirst chamber substantially lower than said initial pressure; and means for minimizing loss of electrons and ions from said stream in said second chamber.
6. Apparatus according to claim 5, wherein said means for causing said ions to drift comprises said gas which by its flow through said apparatus imparts momentum to said ions.
7. Apparatus according to claim 5, wherein said means for causing said ions to drift comprises means for supplying and directing a separate inactive gas through said apparatus for imparting momentum to said ions.
8. Apparatus for producing a beam of low temperature electrons comprising: a source of electrons having a mean thermal velocity determining an initial electron temperature substantially higher than room temperature; a first chamber `and means for supplying a gas thereto having a temperature substantially lower than said initial electron temperature and an initial pressure between 10*5 and l0*1 mm. of Hg; means for causing said electrons to drift through said rst chamber at a drift velocity substantially less than said mean thermal electron velocity, whereby said electrons are cooled to a temperature substantially below said initial electron temperature as a result of collisions with the molecules of said gas; a second chamber communicating with said iirst chamber through which said electrons ydrift after passage through said rst chamber; means for supplying positive ions to said chambers; means for progressively reducing the gas pressure in said second chamber in the direction of electron drift to a pressure at the end thereof remote from said iirst chamber substantially lower than said initial pressure; means for minimizing loss of electrons and ions in said second chamber; and means located at said remote end for separating said positive ions and said electrons and forming said electrons into a beam of low temperature electrons along a desired path.
9. Apparatus according to claim 8, wherein said means for causing said electrons to drift and said last-named means comprise an electron accelerating electrode located at said remote end of said second chamber.
l0. Apparatus for producing a beam of low temperature electrons comprising: a rst chamber and means for supplying a gas thereto having a temperature no higher than room temperature and an initial pressure between 10-5 and 10-l mm. of Hg; means for supplying a stream of electrons and positive ions to said chamber, said electrons having a mean thermal velocity determining an initial electron temperature substantially higher than room temperature; means for causing said electrons and ions to drift through said chamber in the same general direction at a drift velocity substantially less than said mean thermal electron velocity, whereby said electrons and ions are cooled to a temperature substantially below said initial electron temperature as a result of collisions with the molecules of said gas; a second chamber communicating with said rst chamber through which said ions and electrons drift after passage through said irst chamber; means for progressively reducing the gas pressure in said second chamber in the direction of drift to a pressure at the end thereof remote from said rst chamber substantially lower than said initial pressure; means for producing a confining magnetic eld extending along said drift direction; and means located at said remote end for separating said positive ions from said electrons and forming said electrons into a beam of low temperatuire electrons along a desired path.
1l. Apparatus according to claim l0, wherein said gas is ammonia at an initial pressure of about 1 micron of Hg, and said pressure at said remote end of said second chamber is not greater than 10-6 mm. of Hg.
12. A source of electrons and positive ions comprising a member metal having an electron emissive surface with a given work function, means for bombarding said member with electrons to heat said member to electron emitting temperature, land means for supplying at said surface of said member for contact ionization thereat metal vapor atoms having an ionization potential less than said work function, said atoms being provided by continuous evaporation of atoms from an alkaline metal.
13. A source according to claim l2, wherein said member is a plate of tungsten, and said alkaline metal is cesium.
References Cited in the le of this patent UNITED STATES PATENTS 2,798,181 Foster July 2, 1957
US667920A 1957-06-25 1957-06-25 Apparatus for producing thermallycool charged particles Expired - Lifetime US2883568A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US667920A US2883568A (en) 1957-06-25 1957-06-25 Apparatus for producing thermallycool charged particles

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US667920A US2883568A (en) 1957-06-25 1957-06-25 Apparatus for producing thermallycool charged particles

Publications (1)

Publication Number Publication Date
US2883568A true US2883568A (en) 1959-04-21

Family

ID=24680209

Family Applications (1)

Application Number Title Priority Date Filing Date
US667920A Expired - Lifetime US2883568A (en) 1957-06-25 1957-06-25 Apparatus for producing thermallycool charged particles

Country Status (1)

Country Link
US (1) US2883568A (en)

Cited By (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2967257A (en) * 1959-04-24 1961-01-03 Milleron Norman Ion pump
US2977495A (en) * 1958-05-03 1961-03-28 Commissariat Energie Atomique Ion source
US2978580A (en) * 1958-04-25 1961-04-04 Vakutronik Veb Process and device for the addition of slow electrons to polyatomic or highmolecular compounds
US3054896A (en) * 1961-01-12 1962-09-18 William H Jones Apparatus for electron beam heating control
US3063291A (en) * 1959-09-24 1962-11-13 Childs James Howard High-vacuum condenser tank for ion rocket tests
US3119232A (en) * 1960-10-04 1964-01-28 Edward A Richley Rocket engine
US3130542A (en) * 1962-10-26 1964-04-28 United Aircraft Corp Collector for neutral particles
DE1180073B (en) * 1961-01-21 1964-10-22 Euratom Process for generating a straight stream of matter with a density of over 10-g / cm inside a closed high vacuum space
US3173246A (en) * 1963-03-12 1965-03-16 Carl T Norgren Colloid propulsion method and apparatus
US3230419A (en) * 1961-10-30 1966-01-18 Willard H Bennett Means for producing focused high density electron streams
US3253180A (en) * 1961-09-27 1966-05-24 Csf Hollow cathodes
US3255376A (en) * 1962-01-02 1966-06-07 Rca Corp Low-noise electron guns
US3308622A (en) * 1964-07-29 1967-03-14 Electro Optical Systems Inc Ion propulsion system with ion engine utilizing power supply hot surface
US3319118A (en) * 1964-07-16 1967-05-09 Charles C Damm Process and apparatus for producing purified fast particle beams
US3370198A (en) * 1967-06-21 1968-02-20 Kenneth C. Rogers Plasma accelerator having a cooled preionization chamber
US3453489A (en) * 1966-04-27 1969-07-01 Xerox Corp Multiple anode electrode assembly
US3453469A (en) * 1965-05-20 1969-07-01 Xerox Corp Multi-level vacuum pumping system for plasma containment device
US3525013A (en) * 1968-07-26 1970-08-18 Ibm Metallic ion source including plurality of electron guns
US4894511A (en) * 1986-08-26 1990-01-16 Physical Sciences, Inc. Source of high flux energetic atoms
US20090321655A1 (en) * 2006-11-07 2009-12-31 Alexander Makarov Ion Transfer Tube with Spatially Alternating DC Fields
US20100038532A1 (en) * 2006-11-07 2010-02-18 Alexander Makarov Efficient Atmospheric Pressure Interface for Mass Spectrometers and Method
EP2960599A1 (en) * 2014-06-13 2015-12-30 Lockheed Martin Corporation Cooling a target using electrons

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2798181A (en) * 1954-03-26 1957-07-02 Jr John S Foster Pumping ion source

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2798181A (en) * 1954-03-26 1957-07-02 Jr John S Foster Pumping ion source

Cited By (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2978580A (en) * 1958-04-25 1961-04-04 Vakutronik Veb Process and device for the addition of slow electrons to polyatomic or highmolecular compounds
US2977495A (en) * 1958-05-03 1961-03-28 Commissariat Energie Atomique Ion source
US2967257A (en) * 1959-04-24 1961-01-03 Milleron Norman Ion pump
US3063291A (en) * 1959-09-24 1962-11-13 Childs James Howard High-vacuum condenser tank for ion rocket tests
US3119232A (en) * 1960-10-04 1964-01-28 Edward A Richley Rocket engine
US3054896A (en) * 1961-01-12 1962-09-18 William H Jones Apparatus for electron beam heating control
DE1180073B (en) * 1961-01-21 1964-10-22 Euratom Process for generating a straight stream of matter with a density of over 10-g / cm inside a closed high vacuum space
US3253180A (en) * 1961-09-27 1966-05-24 Csf Hollow cathodes
US3230419A (en) * 1961-10-30 1966-01-18 Willard H Bennett Means for producing focused high density electron streams
US3255376A (en) * 1962-01-02 1966-06-07 Rca Corp Low-noise electron guns
US3130542A (en) * 1962-10-26 1964-04-28 United Aircraft Corp Collector for neutral particles
US3173246A (en) * 1963-03-12 1965-03-16 Carl T Norgren Colloid propulsion method and apparatus
US3319118A (en) * 1964-07-16 1967-05-09 Charles C Damm Process and apparatus for producing purified fast particle beams
US3308622A (en) * 1964-07-29 1967-03-14 Electro Optical Systems Inc Ion propulsion system with ion engine utilizing power supply hot surface
US3453469A (en) * 1965-05-20 1969-07-01 Xerox Corp Multi-level vacuum pumping system for plasma containment device
US3453489A (en) * 1966-04-27 1969-07-01 Xerox Corp Multiple anode electrode assembly
US3370198A (en) * 1967-06-21 1968-02-20 Kenneth C. Rogers Plasma accelerator having a cooled preionization chamber
US3525013A (en) * 1968-07-26 1970-08-18 Ibm Metallic ion source including plurality of electron guns
US4894511A (en) * 1986-08-26 1990-01-16 Physical Sciences, Inc. Source of high flux energetic atoms
US20090321655A1 (en) * 2006-11-07 2009-12-31 Alexander Makarov Ion Transfer Tube with Spatially Alternating DC Fields
US20100038532A1 (en) * 2006-11-07 2010-02-18 Alexander Makarov Efficient Atmospheric Pressure Interface for Mass Spectrometers and Method
US20100038533A1 (en) * 2006-11-07 2010-02-18 Makarov Alexander A Ion Transfer Arrangement with Spatially Alternating DC and Viscous Ion Flow
US7982183B2 (en) * 2006-11-07 2011-07-19 Thermo Fisher Scientific (Bremen) Gmbh Ion transfer tube with spatially alternating DC fields
US8148680B2 (en) * 2006-11-07 2012-04-03 Thermo Fisher Scientific (Bremen) Gmbh Ion transfer arrangement with spatially alternating DC and viscous ion flow
US8148679B2 (en) * 2006-11-07 2012-04-03 Thermo Fisher Scientific (Bremen) Gmbh Efficient atmospheric pressure interface for mass spectrometers and method
EP2960599A1 (en) * 2014-06-13 2015-12-30 Lockheed Martin Corporation Cooling a target using electrons
US9933189B2 (en) 2014-06-13 2018-04-03 Lockheed Martin Corporation Cooling a target using electrons
US10935285B2 (en) 2014-06-13 2021-03-02 Lockheed Martin Corporation Cooling a target using electrons

Similar Documents

Publication Publication Date Title
US2883568A (en) Apparatus for producing thermallycool charged particles
US2899556A (en) Apparatus for the treatment of substances
US6740874B2 (en) Ion mobility spectrometer with mechanically stabilized vacuum-tight x-ray window
JP3791783B2 (en) Ion attachment mass spectrometer, ionizer, and ionization method
US7462822B2 (en) Apparatus and method for the transport of ions into a vacuum
US4894546A (en) Hollow cathode ion sources
US2816243A (en) Negative ion source
US2798181A (en) Pumping ion source
US4739214A (en) Dynamic electron emitter
US5899666A (en) Ion drag vacuum pump
US20010016166A1 (en) Plasma vacuum pumping cell
US2737593A (en) Method of irradiating streams of liquids, gases, finely divided solids, etc., by continuous beams of high instantaneous ionization density
US2841726A (en) Apparatus for producing thermallycool charged particles
US3262262A (en) Electrostatic ion rocket engine
US2578009A (en) Electronic high vacuum apparatus
US3022933A (en) Multiple electron beam ion pump and source
US2936393A (en) Low noise traveling-wave tube
JP4571003B2 (en) Cluster ion beam equipment
US3673405A (en) Gas inlet system for a mass spectrometer
US5326227A (en) Exhaust apparatus with vacuum pump
US2967943A (en) Gaseous discharge device
EP0469631B1 (en) Ion pump and vacuum pumping unit using the same
GB1398167A (en) High pressure ion sources
US5240381A (en) Exhaust apparatus and vacuum pumping unit including the exhaust apparatus
US3253402A (en) Apparatus for and method of emitting particles