Plasma Source for Charged Particle Beam System

Abstract

An inductively coupled plasma source for a focused charged particle beam system includes a dielectric liquid that insulates and cools the plasma chamber. A flow restrictor at an electrical potential that is a large fraction of the plasma potential reducing arcing because the voltage drop in the gas occurs primarily at relative high pressure.

Description

TECHNICAL FIELD OF THE INVENTION

The present invention relates to plasma sources used in ion beam columns

BACKGROUND OF THE INVENTION

Inductively coupled (IC) plasma sources have advantages over other types of plasma sources when used with a focusing column to form a focused beam of charged particles, i.e., ions or electrons. The inductively coupled plasma source is capable of providing charged particles within a narrow energy range, which allows the particles to be focused to a small spot. IC plasma sources, such as the one described in U.S. Pat. No. 7,241,361, which is assigned to the assignee of the present invention, include a radio frequency (rf) antenna typically wrapped around a ceramic plasma chamber. The RF antenna provides energy to maintain the gas in an ionized state within the chamber.

The energy of ions used for ion beam processes is typically between 5 keV and 50 keV, and most typically about 30 keV. Electron energy varies between about 500 eV to 5 keV for a scanning electron microscope system to several hundred thousand electron volts for a transmission electron microscope system. The sample in a charged particle system is typically maintained at ground potential, with the source maintained at a large electrical potential, either positive or negative, depending on the particles used to form the beam. The ion or electron source is typically maintained at a high positive or negative voltage, and the sample is typically maintained at or near ground potential. Thus, the ion beam source is typically maintained at between 5 kV and 50 kV and the electron source is typically maintained at between 500 eV and 5 kV. “High voltage” as used herein means positive or negative voltage greater than about 500 eV above or below ground potential. For the safety of operating personnel, it is necessary to electrically isolate the high voltage components. The electrical isolation of the high voltage plasma creates several design problems that are difficult to solve in light of other goals for a plasma source design.

One design difficulty occurs because gas must be brought into the high voltage plasma chamber to replenish the gas as ions leave the plasma. The gas is typically stored at ground potential and well above atmospheric pressure. Gas pressure in a plasma chamber typically varies between about 10⁻³ mbar and about 1 mbar. The electrical potential of the gas must be brought to that of the high voltage plasma and the pressure of the gas must be decreased as the gas moves from the gas source into the plasma chamber. The gas must be brought into the chamber in a way that prevents a gas phase discharge, also known as arcing, which would damage the system.

Another design challenge is to place the radio frequency coils that provide power to the plasma as close as possible to the plasma to efficiently transfer power. Maintaining the coils at the same high potential as the plasma, however, would typically require maintaining the power supply for the coil at the high plasma potential, which would excessively complicate the power supply design and greatly increase the cost. Inductively coupled plasma ion sources may use a split Faraday shield to reduce capacitive coupling between the coil and the plasma. The split Faraday shield must be located between the plasma and the coils and is typically well grounded. When the grounded Faraday shield is located close to the dielectric plasma container, the large electric field caused by the rapid change in potential would likely cause a gas-phase discharge if any air is trapped between the Faraday shield and the dielectric plasma chamber, which discharge could damage the source.

Also, the energy applied to the plasma chamber generates heat. While a compact plasma source is desirable for beam formation, the more compact and powerful the plasma source, the hotter the source would become and therefore the greater the need to efficiently dissipate the heat. The high voltage can also make cooling difficult, which can limit the density of the plasma used. These conflicting requirements make the design of an ICP source very challenging.

SUMMARY OF THE INVENTION

An object of the invention is to provide an improved plasma source and an improved charged particle system having a plasma charged particle beam source.

This invention provides an improved inductively coupled plasma source for a charged particle beam system. In one preferred embodiment, the plasma source is surrounded by a liquid that provides cooling and optionally a portion of the electrical insulation of the plasma chamber. In another embodiment, gas is introduced into the plasma chamber through a flow restrictor maintained at high voltage so that most of the voltage drop between the plasma and the gas supply occurs where the gas is maintained at a higher pressure thereby reducing arcing.

The foregoing has outlined rather broadly the features and technical advantages of the present invention in order that the detailed description of the invention that follows may be better understood. Additional features and advantages of the invention will be described hereinafter. It should be appreciated by those skilled in the art that the conception and specific embodiments disclosed may be readily utilized as a basis for modifying or designing other structures for carrying out the same purposes of the present invention. It should also be realized by those skilled in the art that such equivalent constructions do not depart from the spirit and scope of the invention as set forth in the appended claims.

BRIEF DESCRIPTION OF THE DRAWINGS

For a more thorough understanding of the present invention, and advantages thereof, reference is now made to the following descriptions taken in conjunction with the accompanying drawings, in which:

FIG. 1 shows a longitudinal cross-sectional schematic view of a plasma source that uses an insulating liquid for high voltage isolation and cooling.

FIG. 2 shows a transverse cross-sectional schematic view of the plasma source of FIG. 1.

FIG. 3 shows changed particle beam system that uses a plasma source which uses an insulating liquid for cooling and high voltage isolation.

DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS

Designing a plasma source typically requires many tradeoffs to meet conflicting design requirements. Embodiments of the invention can provide excellent coupling between the rf coil and the plasma, efficient cooling of the plasma chamber, excellent capacitive screening, and high voltage isolation of the plasma source all of which can produce an inductively coupled plasma that is dense, quiescent, and at high potential.

In some embodiments, expelling gas from regions with strong electric fields and filling those volumes with fluid provides a system designer the opportunity to make design choices with regard to the source configuration that would be otherwise unavailable to him

The description below describes a plasma source for a focused ion beam system, but a plasma source of the present invention can be used for an electron beam system, or other system.

FIG. 1 shows a longitudinal cross-sectional view of a stylized plasma source 100 embodying aspects of the invention. The plasma source 100 includes a dielectric plasma chamber 102 having an interior wall 104 and an exterior wall 106. Plasma chamber 102 rests on a conductive base plate 110. A plasma 112 is maintained within the plasma chamber 102. Extraction optics 114 extract charged particles, ion or electrons depending on the application, from plasma 112 through an opening 116 in plasma chamber 102 and opening 118 in base plate 110. A dielectric outer shell 120, preferably of ceramic or plastic material that transmits radio frequency energy with minimal loss, is concentric with plasma chamber 102 and defines a space 122 between outer shell 120 and plasma chamber outer wall 106. A pump 124 pumps an cooling fluid 126 from a reservoir/chiller 127 to space 122 through cooling fluid inlets 128 and exit through exit 132, cooling plasma chamber 102 by thermal transfer from outer wall 106.

Because the electrical potential drops rapidly between the plasma region and the split Faraday shield, materials between the plasma region and the split Faraday shield must have sufficiently large dielectric strength to resist arcing. The cooling fluid can be chosen to have a sufficiently high dielectric constant compared to the material of ceramic housing 102 so that the voltage drop across the liquid is sufficiently low to prevent dielectric breakdown at the operating voltage. In this case the coolant is also chosen to be free of gaseous bubbles or other impurities which could present the opportunity for field enhancement and gaseous electric discharge. The cooling fluid can also be chosen to be slightly conductive in which case the fluid volume will be substantially free of electric fields and substantially all of the voltage drop will take place in the plasma chamber 102. The cooling fluid should also have sufficient heat capacity to prevent the plasma chamber 102 from overheating without requiring a large fluid flow that requires a large pump that would consume excessive power. The plasma chamber 102 is typically maintained at a temperature of less than about 50 C.

The fluid preferably comprises a liquid, such as water or Fluorinert™ FC-40, an electrically insulating, stable fluorocarbon-based fluid from sold commercially by 3M Company, St. Paul, Minn. Water, such as deionized water or tap water, may be used. A preferred pumps the cooling fluid at a rate of between 10 gal/hour and 50 gal/hour from reservoir/chiller 127. Fluid 126 returns from exit 132 to chiller/reservoir 127 via a return conduit 133. Water has a dielectric constant of about 80, whereas the ceramic material of the plasma chamber has a dielectric constant of about 9, which results in most of the voltage drop occurring in the ceramic. A preferred insulating liquid has a dielectric constant preferably greater than that of the dielectric material of which the plasma chamber is made. In some embodiments, the insulating liquid has a dielectric constant greater than 5, more preferably greater than 10, even more preferably greater than 20, and most preferably greater than or equal to about 40.

In a typical embodiment, reservoir/chiller 127 cools the cooling fluid to about 20° C. before the fluid is recirculated by pump 124. The cooling fluid partly surrounds the plasma chamber and the coolant flows longitudinally along the plasma chamber from bottom to top. For clarity, FIG. 1 shows cooling fluid entering space 122 on two sides at the bottom of plasma chamber 102 and exiting space 122 one on side at the top of chamber 102. Skilled persons will understand that suitable inlets, outlets, and baffles may be used to ensure an even fluid flow around all sides of the plasma chamber 102.

A split Faraday shield 134 passes the radio frequency energy from rf coils 136 to energize the plasma while reducing the capacitive coupling between radio frequency coils 136 and plasma 112. Split faraday shield 134 includes slits to reduce eddy currents induced by rf coils 136. RF coils 136 may be hollow and cooled by flow of a coolant through the internal passages 137 in the coils. The plasma chamber coolant system may also pump coolant through the coils, or the coils can have an independent cooling system.

Faraday shield 134 is preferably positioned such that cooling fluid 126 flows on both sides of the shield 134 and can flow between slits in the shield to contact . Alternatively, the shield can be positioned against the outer wall 106 or onto the inside wall of shell 120. For example, the shield can comprise a metallic layer painted or otherwise deposited on outer plasma chamber wall 106 or inside shell wall 120. Faraday shield is electrically grounded. In one embodiment, shield 134 comprises a metal cylinder that is grounded by trapping a tab 138 of the Faraday shield between a portion of outer shell 120 and base plate 110, thereby ensuring a solid ground contact.

The gas must be brought from ground potential to the plasma potential along the path between the tank 150 and the plasma. In a preferred embodiment, most of the voltage change occurs where the gas pressure is relatively high and resistant to arcing.

Gas is provided to plasma chamber 102 from a gas source, such as a tank 150. Tank 150 is typically maintained at ground potential and contains the gas at a high pressure. A regulator 152 reduces the pressure of the gas leaving the tank entering a conduit 154. An optional adjustable valve 156 further reduces the pressure in the gas line or closes the conduit completely when the source is not in use. A flow restrictor, such as a capillary 158, further reduces the gas pressure before the gas reaches plasma chamber 106. Restrictor 158 provides a desired gas conductance between the gas line and the interior of plasma chamber 102. Restrictor 158 is preferably in electrical contact with plasma 112 and so is at the plasma potential. In other embodiments, the flow restriction can have an electrical bias applied from a voltage source other than the plasma. An insulating shield 160 surrounds capillary 158 and a grounded metallic collar 162 at the end of insulating shield 160 ensures that the electrical potential of the gas is zero at that position. Thus, the entire electrical potential change from ground to the plasma voltage occurs within insulating shield 160 in which the gas is at a relatively high pressure and therefore resistant to arcing.

In one example embodiment without a valve 156, regulator 152 reduces the pressure of the gas leaving the supply tank 150 to 5 psig. The gas pressure remains at 5 psig until the gas reaches capillary 158, and which point the gas pressure drops to the plasma chamber pressure of, for example, 0.1 Torr. Insulating shield 160 preferably has sufficient length to keep the field sufficiently low to prevent a damaging discharge. Insulating shield 160 is typically about at least about 5 mm long, and more typically between about 30 mm and 60 mm For example, if the plasma is maintained at 30 kV, the electric field within a 10 mm shield is about 3 kV/mm, which is sufficiently low to prevent a sustained discharged in most applications. Skilled persons will understand that the local electric field will be a function of the geometry and that initial low current discharges may occur to reach a static charge equilibrium within insulating shield 160. In some embodiments, valve 156 may reduce the gas pressure further before the gas reaches the final restrictor before the plasma. Instead of a capillary, the flow restrictor could be a valve, such as a leak valve. Any type of gas source could be used. For example, the gas source may comprise a liquid or solid material that is heated to produce gas at a sufficient rate to supply the plasma. The different output pressures of the different gas sources may require different components to reduce the pressure to that required in the plasma chamber.

FIG. 2 shows a transverse cross-sectional view of plasma source 100 in FIG. 1. FIG. 2 shows that the outer wall 106 of plasma chamber 102 is corrugated, that is, it is composed of a series of ridges 202 and valleys 204. The Faraday shield 134 is positioned against the ridges 202, defining passages 206 for the cooling fluid to flow between the valleys 204 and the shield 134. In the embodiment shown in FIG. 2, the Faraday shield 134 comprises a metal sleeve that slips over plasma chamber outer wall 106. A portion of the metal sleeve is then bent outward at the bottom to form grounding tab 138 (FIG. 1), which is trapped between plasma chamber 102 and ground plate 110. Cooling fluid 126 flows through the space 122 which is bounded by the plasma chamber outer wall 106 and the shell 120. The Faraday shield is “split,” that is, there are vertical slots in the shield, which allow the cooling fluid to pass. In an alternative embodiment, the outer wall 106 may be smooth and the Faraday shield formed with corrugations. Alternatively, neither the wall 106 nor the faraday shield may be corrugated.

FIG. 3 shows a charged particle beam that uses the plasma source of FIG. 1. At the top of the ion column, an inductively-coupled plasma (ICP) ion source 302 is mounted, comprising an electromagnetic enclosure 304, a source chamber 306, and an induction coil 308, which includes one or more winds of a conductive material. A coolant reservoir and chiller 390 supplies provides coolant to a pump 391, which provides coolant by conduit 392 to a coolant region around source chamber 306. The coolant then flows back to coolant reservoir and chiller 390 through a return conduit 393.

A radio frequency (RF) power supply 340 is connected to a match box 341 by two radio frequency (RF) coaxial cables 342. The match box 341 is connected to the induction coil 308 by two RF coaxial cables 343. The induction coil 308 is mounted coaxially with the source chamber 306. To reduce capacitive coupling between the induction coil 308 and the plasma generated within the source chamber 306, a split Faraday shield (not shown) may optionally be mounted coaxially with the source chamber 306 and inside the induction coil 308. When a split Faraday shield is used in the ICP ion source 302, the high voltage (typically several hundred volts) across the induction coil 308 will have minimal effect on the energies of the ions extracted from the bottom of the ICP ion source 302 into the ion column. This will result in smaller beam energy spreads, reducing the chromatic aberration in the focused charged particle beam at or near the substrate surface.

The presence of a plasma within the source chamber 306 may be detected using the light emitted by the plasma and collected by the source-facing end of optic fiber 344, and transmitted through optic fiber 344 to a plasma light detection unit 345. An electrical signal generated by the plasma light detection unit 345 is conducted through cable 346 to a programmable logic controller (PLC) 347. The plasma on/off signal generated by the plasma light detection unit 345 then passes from the PLC 347 through cable or data bus 348 to the plasma source controller 351 executing plasma source control software. Signals from the plasma source controller 351 may then pass through cable or data bus 352 to the focused ion beam (FIB) system controller 353. The FIB system controller 353 may communicate via the Internet 354 to a remote server 355. These details of the interconnections of the various components of the FIB system control are for exemplary purposes only. Other control configurations are possible as is familiar to those skilled in the art.

Gas is provided to the source chamber 306 by inlet gas line 320 which leads to inlet restrictor 328, which leads to the interior of the source chamber 306. Restrictor 328 is maintained at an electrical potential closer to the potential of the plasma in chamber 306 than to the potential of the gas source 310 and regulator 332 so that the voltage drop occurs primarily across gas of higher pressure. Insulating shield 329 insulates the gas line upstream of restrictor 328 and is terminated with a grounded collar 331.

A gas supply system 310 for the ICP source comprises a gas supply 330, a high purity gas regulator 332, and a needle (regulating) valve 334. The gas supply 330 may comprise a standard gas bottle with one or more stages of flow regulation, as would be the case for helium, oxygen, xenon or argon feed gases, for example. Alternatively, for gases derived from compounds which are solid or liquid at room temperature, gas supply 330 may comprise a heated reservoir. Other types of gas supplies 330 are also possible. The particular choice of gas supply 330 configuration is a function of the type of gas to be supplied to the ICP source. Gas from supply 330 passes through high purity gas regulator 332, which may comprise one or more stages of purification and pressure reduction. The purified gas emerging from high purity gas regulator 332 passes through an optional needle valve 334. Gas emerging from optional needle valve 334 passes through a hose 336 to an optional second needle valve 338, mounted in close proximity to the ICP source. Gases emerging from needle valve 338 pass through inlet gas line 320, which connects through restriction 328 to the top of the source chamber 306.

At the bottom of the ICP source 302, a source electrode 357 serves as part of the ion beam extraction optics, working in conjunction with the extractor electrode 358 and the condenser 359. A plasma igniter 360 is connected to a source electrode (not shown), enabling the starting of the plasma in the source enclosure 306. Other known means of igniting the plasma can also be used. Details of the operation of the ICP source are provided in U.S. Pat. No. 7,241,361, issued Jul. 10, 2007, incorporated by reference herein. The source electrode 357 is biased through the igniter 360 to a high voltage by beam voltage power supply (PS) 361. The voltage on the source electrode 357 determines potential of the plasma and therefore the energy of the charged particles reaching the substrate surface in the case of singly-ionized atomic or molecular ion species or electrons. Doubly-ionized ion species will have twice the kinetic energy. The extractor electrode 358 is biased by extractor power supply 363, while the condenser 359 is biased by condenser power supply 362. The combined operation of the source electrode 357, the extractor 358, and the condenser 359 serves to extract and focus ions emerging from the ICP source 302 into a beam which passes to the beam acceptance aperture 364. The beam acceptance aperture 364 is mechanically positioned within the ion column by the beam acceptance aperture actuator 365, under control of the FIB system controller 353. Typical voltage settings may be roughly +30 kV for power supply 361, roughly 15 kV for power supply 362 and roughly 15 kV for power supply 363.

The ion column illustrated in FIG. 3 shows two electrostatic einzel lenses 366 and 367, used to form a highly demagnified (roughly 1/125×) image of the virtual source in the ICP source 302 at or near the surface of substrate 368, mounted on stage 369 controlled by a sample stage controller 337. The first einzel lens, 366, referred to as “lens 1” or “L1,” is located directly below the beam acceptance aperture 364 and comprises three electrodes with the first and third electrodes typically being grounded (at 0V), while the voltage of the center electrode 370 is controlled by lens 1 (L1) power supply (PS) 371. The lens 1 power supply 371 is controlled by the FIB system controller 353.

Between the first einzel lens 366 and the second einzel lens 367 in the ion column, a beam defining aperture assembly 372 is mounted, comprising one or more beam defining apertures (three apertures are shown in FIG. 3). Typically, the beam defining aperture assembly 372 would comprise a number of circular apertures with differing diameter openings, where any one of which could be positioned on the optical axis to enable control of the beam current and half-angle at the substrate surface. Alternatively, two or more of the apertures in the beam defining aperture assembly 372 may be the same, thereby providing redundancy to enable the time between aperture maintenance cycles to be extended. By controlling the beam half-angle, the beam current and diameter of the focused ion beam at or near the substrate surface may be selected, based on the spatial resolution requirements of the milling or imaging operations to be performed. The particular aperture to be used (and thus the beam half-angle at the substrate) is determined by mechanical positioning of the desired aperture in the beam defining aperture assembly 372 on the optical axis of the column by means of the beam defining aperture (BDA) actuator 373, controlled by the FIB system controller 353.

Beneath the beam defining aperture assembly 372, the second einzel lens 367, referred to as “lens 2” or “L2,” is shown. The first and third electrodes are typically grounded (0 V), while the voltage of the center electrode 374 is controlled by lens 2 (L2) power supply (PS) 375. The lens 2 power supply 375 is controlled by the FIB system controller 353. A column/chamber isolation valve 376 is positioned somewhere between the source 302 and the sample chamber 378. Isolation valve 376 enables the vacuum in the ion column vacuum chamber 377 to be maintained at high levels, even if the vacuum level in the sample chamber 378 is adversely affected by sample outgassing, during sample introduction and removal, or for some other reason. A column/chamber turbopump 379 is configured to pump the sample chamber 378 through a pumping line 380. Turbopump 379 also pumps the ion column enclosure 377 through pumping line 381.

The details of the FIB system illustrated in FIG. 3 are for exemplary purposes only—many other FIB system configurations are capable of implementing a multiple mode embodiment of the present invention for milling and imaging. For example, the ion column illustrated in FIG. 3 shows two electrostatic einzel lenses. The ion column may alternatively be implemented using a single electrostatic einzel lens, or more than two electrostatic lenses. Other embodiments might include magnetic lenses or combinations of two or more electrostatic or magnetic quadrupoles in strong-focusing configurations. For the purposes of this embodiment of the present invention, it is preferred that the ion column forms a highly demagnified image of the virtual source (in the ICP source 302) at or near the surface of the substrate 368. Details of these possible demagnification methods are familiar to those skilled in the art.

Although the present invention and its advantages have been described in detail, it should be understood that various changes, substitutions and alterations can be made to the embodiments described herein without departing from the spirit and scope of the invention as defined by the appended claims. Moreover, the scope of the present application is not intended to be limited to the particular embodiments of the process, machine, manufacture, composition of matter, means, methods and steps described in the specification. As one of ordinary skill in the art will readily appreciate from the disclosure of the present invention, processes, machines, manufacture, compositions of matter, means, methods, or steps, presently existing or later to be developed that perform substantially the same function or achieve substantially the same result as the corresponding embodiments described herein may be utilized according to the present invention. Accordingly, the appended claims are intended to include within their scope such processes, machines, manufacture, compositions of matter, means, methods, or steps.

Claims

1. A charged particle beam system, comprising: a plasma source having: a plasma chamber having a wall composed of a dielectric material, the wall having an interior surface and an exterior surface;a conductive film applied to the external surface of the plasma chamber;a conductor coiled at least one time around the plasma chamber;a liquid surrounding at least a portion of the plasma chamber, a portion of the liquid being positioned between the plasma chamber and the conductor; anda source electrode for electrically biasing a plasma in the plasma chamber to a high voltage; andone or more focusing lenses for focusing charged particles from the plasma source onto a sample.

2. The charged particle beam system of claim 1 in which the source electrode for electrically biasing the plasma to a high voltage biases the plasma to a voltage having a magnitude of between 500 eV and 50 keV.

3. The charged particle beam system of claim 1 in which the source electrode for electrically biasing the plasma to a high voltage biases the plasma to produce a landing energy of the charged particles of between 1 keV and 50 keV at the sample.

4. The charged particle beam system of claim 1 in which in operation the plasma in the plasma chamber is maintained at an electrical potential different from ground potential.

5. The charged particle beam system of claim 1 in which the liquid comprises water.

6. The charged particle beam system of claim 1 in which the liquid comprises a fluorine compound.

7. The charged particle beam system of claim 1 in which the conductive film or the external wall of the plasma chamber includes indentations providing a path for the liquid.

8. The charged particle beam system of claim 1 in which the conductive film contains perforations.

9. The charged particle beam system of claim 1 further comprising a metallic base plate in electrical contact with the conductive film.

10. The charged particle beam system of claim 1 in which the liquid has a dielectric constant of greater than 5.

11. The charged particle beam system of claim 1 in which the conductor includes internal passages for passage of the liquid.

12. The charged particle beam system of claim 1 further comprising: a gas source for providing a gas at pressure above atmospheric pressure and at an electrical potential near ground potential; anda flow restrictor for reducing the pressure of the gas before the gas entered the plasma chamber, the flow restrictor being maintained at an electrical potential magnitude greater than ground potential to reduce arcing as the gas approaches the electrical potential of the plasma.

13. The charged particle beam system of claim 12 in which the flow restrictor is maintained at the same electrical potential as the plasma.

14. The charged particle beam system of claim 12 in which the flow restrictor is maintained at an electrical potential having a magnitude greater than ½ the magnitude of the electrical potential of the plasma.

15. A method of operating an inductively coupled plasma source including a plasma chamber surrounded by at least one conductive coil, comprising: providing a plasma chamber having a conductive film on the plasma chamber exterior surface to reduce capacitive coupling between the at least one conductive coil and the plasma;providing radio frequency energy into a plasma chamber from the at least one conductive coil to maintain a plasma in the plasma chamber;maintaining the plasma at an electrical potential different from ground potential;providing a coolant fluid to cool the plasma chamber walls, at least some of the coolant being between the conductive film and the at least one conductive coil so that at least some of the voltage drop between the at least one conductive coil and ground occurs across the liquid;extracting charged particles from the plasma chamber; andfocusing the charged particles into a beam and directing the beam onto or near a work piece, the charged particles having an energy of between 1 keV and 50 keV at the work piece.

16. The method of claim 15 in which providing the coolant fluid to cool the plasma chamber walls includes providing a coolant having a dielectric constant greater than about 20.

17. A method of operating an inductively coupled plasma source including a plasma chamber surrounded by at least one conductive coil, comprising: providing radio frequency energy into a plasma chamber from the at least one conductive coil to maintain a plasma in the plasma chamber;providing a plasma gas at a gas supply pressure and at substantially ground electrical potential;reducing the gas pressure from the gas supply pressure to a plasma chamber entry pressure, the gas pressure being reduced by a flow restrictor having an electrical potential magnitude substantially greater than ground potential to reduce arcing in the delivery of the gas to the plasma chamber;extracting charged particles from the plasma chamber; andfocusing the charged particles into a beam and directing the beam onto or near a work piece.

18. The method of claim 17 in which the flow restrictor is maintained at the same electrical potential as the plasma.

19. The method of claim 17 in which the flow restrictor is maintained at an electrical potential having a magnitude greater than ½ the plasma potential.

20. A plasma source for a charged particle beam system, comprising: a plasma chamber having a wall composed of a dielectric material;a conductor coiled at least one time around the plasma chamber;a plasma electrode for maintaining plasma in the plasma chamber at a high positive or negative voltage relative to ground potential;a gas source for providing a gas at pressure above atmospheric pressure and at an electrical potential near ground potential; anda flow restrictor for reducing the pressure of the gas before the gas entered the plasma chamber, the flow restrictor being maintained at an electrical potential magnitude greater than ground potential and less than the magnitude of the high positive or negative voltage at which the plasma is maintained to reduce arcing as the gas approaches the electrical potential of the plasma.

21. The charged particle beam system of claim 20 in which the flow restrictor comprises a capillary.

22. The charged particle beam system of claim 20 in which the flow restrictor comprises an adjustable leak valve.

23. The charged particle beam system of claim 1 in which the conductive film applied to the external surface of the plasma chamber comprises a metallic layer deposited onto the external surface of the plasma chamber.

24. The charged particle beam system of claim 23 in which the conductive film comprises a metallic layer painted onto the external surface of the plasma chamber.

25. The method of claim 15 in which providing a plasma chamber having a conductive film on the plasma chamber exterior surface includes providing a plasma chamber having a metallic layer deposited onto its external surface.

26. The method of claim 25 in which providing a plasma chamber having a conductive film having a metallic layer deposited onto its external surface includes providing a plasma chamber having a metallic layer painted onto its external surface.