The Ion Sources Sources The ISIS ISIS Penning Penning Ion Ion Source Source and and the the Volume Volume Ion − from from Frankfurt Frankfurt and and DESY DESY for for H H" Production Production # @ J. J. Peters Peters@ J. W. W. G. G. Thomason*, Thomason*, H. H. Klein Klein*,, J. * CLRC RAL, Didcot, *CLRCRAL, Didcot, Oxon, Oxon, UK UK # #IAP, Germany @ IAP, Germany @DESY, Germany DESY, Germany − Abstract. the Institut Institut fur für Angewandte Angewandte Abstract. HH~ ion ion source source development development work work atat Rutherford Rutherford Appleton Appleton Laboratory Laboratory (RAL), (RAL), the Physik (IAP) in Frankfurt and the Deutsches Elektronen-Synchrotron (DESY) will be described, along with future future Physik (IAP) in Frankfurt and the Deutsches Elektronen-Synchrotron (DESY) will be described, along with avenues ion source will be be presented presented in in the the context context avenuesofofresearch. research. The The most most recent recent values values of of important important parameters parameters for for each each ion source will of Source (ESS). (ESS). A A brief brief progress progress of next next generation generation particle particle accelerators, accelerators, particularly particularly the the proposed proposed European European Spallation Spallation Source report RAL ion ion source source measurements measurements were were taken, taken, will willbe beincluded. included. reporton onthe the ISIS ISIS RFQ RFQ test test stand, stand, on on which which many many of of the the RAL INTRODUCTION INTRODUCTION r AA key key element element in in the the design design of of the the ESS ESS is is the the ion ion source for producing pulsed currents at relatively source for producing pulsed currents at relatively high high duty duty cycles. cycles. The The minimum minimum requirement requirement for for the the ESS ESS− short pulse option is a source delivering a 60 short pulse option is a source delivering a 60 mA mA H FT ion ion beam beam inin 1.0 1.0ms ms pulses pulses atat aa repetition repetition rate rate of of 50 50 Hz Hz (5% (5% duty duty cycle) cycle) and and with with aa low low normalised normalised rms rms emittance ~ 0.1 π mm mrad (although emittance ~ 0.1 71 mm mrad (although aa normalised normalised rms rms emittance emittance of of0.2 0.2–- 0.3 0.3πnmm mmmrad mrad at at the the entrance entrance − to the RFQ would be acceptable). If H ions to the RFQ would be acceptable). If FT ions are are also also to to be used for the ESS long pulse option a similar source be used for the ESS long pulse option a similar source will will be be required, required, but but delivering delivering 2.0 2.0 ms ms pulses pulses at at aa repetition rate of 50/3 Hz (3.3% duty cycle). repetition rate of 50/3 Hz (3.3% duty cycle). In addition addition to to meeting meeting these these requirements requirements these these sources sources 1 must mustoperate operate with withhigh high availability availability and and reliability reliability1. ICffliflni a FIGURE cross section section of of the the Frankfurt Frankfurt H~ H− FIGURE 1. 1. Schematic Schematic cross volume volume source. source. As a result of these experiments, experiments, the the ion ion source source 3 shown in figure 1 has been chosen for further study figure chosen for further study3.. The plasma chamber of the the ion ion source source isis made made of of aa water-cooled copper cylinder 7.0 7.0 cm in in diameter diameter and and 10.0 is surrounded surrounded by by ten ten CoSm CoSm 10.0 cm in depth. It is magnets in cusp field field arrangement. Near the the chamber chamber axis are mounted four four tungsten filaments filaments of of 1.8 1.8 mm mm diameter. The front front end of the the chamber chamber is is enclosed enclosed by by the plasma electrode. An electromagnet electromagnet isis installed installed in in the flange of the plasma electrode. Its transverse flange the plasma electrode. Its transverse magnetic field electron filter. filter. An An field (Bff) acts as an electron external oven for introducing introducing caesium caesium isis mounted mounted on on the flange flange of the plasma electrode. electrode. − ItIt has has been been recognised recognised that that no existing H FT ion source sourcecan can immediately immediately fulfil fulfil the the needs needs of the the ESS, ESS, but that a source to meet the minimum requirements could that a source to meet the minimum be developed from present technologies within be developed from present technologies within the 1, 2 time the time scale scale of of building building the the ESS ESS1' . Two types, the volume volume source source and and the the Penning Penning source, source, have been confirmed confirmed as assuitable suitable candidates candidates for for development. development. THE THEFRANKFURT FRANKFURT VOLUME VOLUME SOURCE SOURCE The The low low electron electron temperature temperature and and the the high high achievable achievable current current densities densities which which characterise characterise volume volume sources sources make make them them one one of of the the candidates candidates for for the the ESS injector. Several Several source source prototypes prototypes have have been been used in experiments atatIAP IAP in in Frankfurt Frankfurt to to test test different different source source experiments geometries and and methods methods of of plasma plasma confinement, confinement, and and geometries tooptimise optimise the the cathode cathode configuration. configuration. to The electron is extracted extracted along along with with electron beam which is the H behind the the extractor extractor at at full full FT− ions is dumped behind energy into a water-cooled water-cooled cup. cup. The The extension extension of of the the filter magnet field filter field into the extraction extraction gap gap deflects deflects the the electron beam out of the the beam beam axis axis and and an an additional additional transverse magnetic field field (Bss) is is then then used used to to steer steer the the electron beam into the dumping tube. tube. CP642, High Intensity and High Brightness Hadron Beams: 20th ICFA Advanced Beam Dynamics Workshop on High Intensity and High Brightness Hadron Beams, edited by W. Chou, Y. Mori, D. Neuffer, and J.-F. Ostiguy © 2002 American Institute of Physics 0-7354-0097-0/02/$ 19.00 293 Experiments have shown that, in operation with caesium, the ion source is capable of producing 120 mA of IT beam, measured using a Faraday cup, at an arc power of 47.5 kW (50 Hz, 1.2 ms). With caesium the IT emission current is up to 4.5 times higher, and the e/IT ratio is about 7 at 47.5 kW. The emittance of the source has yet to be measured, but other beam diagnostics have provided a plausible estimate that the normalised rms emittance should be < 0.1 n mm mrad. With the present filament configuration the ion source has been run for 180 hours at an arc power of 40 kW, during which the diameter of the filaments was reduced from 1.8 mm to 1.5 mm. Since the filaments can be used down to a thickness of about 0.9 mm the ion source lifetime could be expected to be about 15 days. Caesium is injected on demand only, so there is wear of the caesium layer, which has to be rebuilt every 10 to 18 hours, requiring a reduction in the arc power for about 15 minutes. A caesium injection system will be developed that will allow caesium injection at higher powers. FIGURE 2. The DESY volume source with A12O3 antenna cover. An investigation of the production of an rf-driven version of the Frankfurt volume source using an external antenna based on the DESY design is planned as part of a European initiative on negative ion sources5, and may provide a source for ESS with enhanced lifetimes. The first phase of this study has shown that the Frankfurt volume ion source has the potential to fulfil the requirements for ESS, but further research and development is required to improve the lifetime and demonstrate the reliability of the source. THE ISIS PENNING SOURCE The ISIS ion source in operation at RAL is shown in figure 3. It is a surface plasma ion source of the Penning type, and routinely produces 35 mA of IT ions (50 Hz, 200|is for uninterrupted periods of up to 50 days6'7. Caesium is used to enhance the production of H~ ions by lowering the work function of the cathode surface. In non-operational periods of ISIS the source has delivered 55 mA for sustained periods in its present form, which corresponds to a current density of ~ 1 A cm"2, which is considerably higher than is possible in volume sources. The e/IT ratio is ~ 1 and so a relatively low electron current is extracted simultaneously with the IT ion beam. The ISIS source has slit extraction geometry, but the extracted beam is immediately passed through a 90° sector magnet with gradient n=l, which separates out any electrons and produces an approximately round beam profile. THE DESY VOLUME SOURCE The DESY rf-driven volume source was developed from a design from Lawrence Berkeley National Laboratory, but incorporating an antenna situated at the wall of the source, completely covered by an Al2Os ceramic4, as shown in figure 2. By removing the antenna from the discharge chamber it is protected from sputtering damage, and so antenna lifetime no longer presents a limit to source performance. The DESY source has now been run for more than 25,000 hours with no antenna failure. In normal operation, without the addition of caesium, the source produces 48 mA of tT ions (10 Hz, 150|is) with a normalised rms emittance of 0.2 n mm mrad. A collar has been introduced into the source for electron suppression, and considerable effort has gone into the optimisation of its geometry, bias and material. With this collar in place an tT current of 80 mA has been reached. A dedicated ion source development rig (ISDR) has been built at RAL that will allow further development of the source to meet the duty cycle and intensity requirements of the ESS8. The ISDR will allow extraction at energies greater than the present 18 keV and emittance measurements to be made close to the source. 294 ion ionbeam beam ion beam extractor extractor extractor introduced IfIf this proves ineffective introduced most most efficiently. efficiently. If this proves proves ineffective ineffective aaa introduced most efficiently. this scaling approach similar to that previously adopted on scaling approach similar to that previously adopted on scaling approach similar to that previously adopted on 99 the 4X and 8X sources at Los Alamos 9 may be the 4X and 8X sources at Los Alamos the 4X and 8X sources at Los Alamos may be adopted, component dimensions has adopted, where where increasing increasing component component dimensions dimensions has has adopted, where increasing been shown to offset heating effects. been shown to offset heating effects. been shown to offset heating effects. The ion source results at RAL have The most most recent recent ion ion source source results results at at RAL RAL have have The most recent 10 10 been produced on the ISIS RFQ test stand have 10 and been produced on the ISIS RFQ test stand and been produced on the ISIS RFQ test stand and have demonstrated rms emittances of 0.16 demonstrated normalised normalised rms rms emittances emittances of of εε8HHH=== 0.16 0.16 demonstrated normalised ππnmm mrad and ε = 0.24 π mm mrad for the standard mm mrad and e = 0.24 n mm mrad for the standard V mm mrad and εVv= 0.24 π mm mrad for the standard ISIS pulse of 200 µs at 35 mA ISIS source source with with aaa beam beam pulse pulse of of 200 200 µs |is at at ≈≈~ 35 35mA mA ISIS source with beam (figure 4). In addition the solenoid matching system (figure 4). In addition the solenoid matching system (figure 4). In addition the solenoid matching system has excellent matching into the has been been shown shown to to provide provide excellent excellent matching matching into intothe has been shown to provide RFQ, allowing transmission factors through the RFQ RFQ, allowing transmission factors through the RFQ, allowing transmission factors through the RFQ of, an input current of 36 mA. of, typically, typically, 91% 91% for for an an input input current current of of 36 36 mA. mA. of, typically, 91% for Further and development of the Penning Further research research and and development development of of the the Penning Penning Further research source is needed to meet the ESS specifications, but source is needed to meet the ESS specifications, source is needed to meet the ESS specifications, but this is not a large extrapolation from current this is not a large extrapolation from current this is not a large extrapolation from current performance considered feasible in the performance and and is considered feasible feasible in in the the performance and isis considered timescale timescaleof ofthe the ESS. ESS. timescale of the ESS. aperture apertureplate plate aperture plate discharge dischargeregion region discharge region Penning PenningBB Bfield field Penning field anode anode anode source sourcebody body source body ceramic ceramic cathode cathode cathode 10 mm 10mm 10 mm mica mica mica flange flange flange copper copperdisc disc copper disc FIGURE FIGURE3.3. 3.Schematic Schematicof ofthe theISIS ISISion ionsource. source. FIGURE Schematic of the ISIS ion source. horizontal horizontalemittance emittance54−216 54-216µs \LS horizontal emittance 54−216 µs 100 100 100 εε ==0.16 0.16ππmm mmmrad mrad ACKNOWLEDGMENTS ACKNOWLEDGMENTS ACKNOWLEDGMENTS rms rms x′ (mrad) x′ (mrad) 50 50 50 The like to thank K. Volk and R. The authors authors would would like like to to thank thank K. K. Volk Volk and and R. R. The authors would Sidlow contributions to ion source Sidlow for for invaluable invaluable contributions contributions to to ion ion source source Sidlow for invaluable development at at IAP IAP and and RAL, RAL, respectively, respectively, and and A. A. P. P. development and RAL, respectively, and A. P. development at IAP Letchford and C. P. Bailey for data from the Letchford and C. P. Bailey for data from the ISIS RFQ Letchford and C. P. Bailey for data from the ISIS RFQ teststand. stand. test test stand. 00 -50 −50 −50 -100 −100 −100 −6 −6 −2 −2 −4 −4 2 00 0 (mm) xxx(mm) (mm) REFERENCES REFERENCES 2 22 44 66 Ferdinand, R., R., Klein, Klein, H. H. and and Thomason, Thomason, J. J. W. 1.1. Ferdinand, J. W. G., G., ESS ESS Workshop on on Sources, Sources, 28 28 November November 2001, 2001, Saclay, Saclay, ESS ESS Workshop 2001, Saclay, ESS report,(April (April2002) 2002) report, verticalemittance emittance54−216 54-216µs ^s vertical vertical emittance 54−216 µs 100 100 100 εrms 0.24ππmm mmmrad mrad ε ==0.24 Schroder,L., L.,Leung LeungK-N., K-N.,and andAlonso, Alonso,J.J.(Ed.), (Ed.),Proc. Proc.of of 2.2. Schröder, (Ed.), Proc. of Workshop on on Ion Ion Source Source Issues Issues Relevant Relevant to to aaa Pulsed Pulsed Workshop Relevant to Pulsed Spallation Neutron Neutron Source, Source, Lawrence Lawrence Berkeley Berkeley Spallation Lawrence Berkeley NationalLaboratory, Laboratory, USA, USA, (1994). (1994). National rms y′ (mrad) y′ (mrad) 50 50 50 00 Volk, K., K., Maaser, Maaser, A. A. and and Klein, Klein, H., H., LINAC LINAC 98, 98, 3.3. Volk, H., LINAC 98, TH4057(1998). (1998). TH4057 -50 −50 −50 -100 −100 −100 Peters,J., J.,RSI RSI69(2), 69(2),(1998). (1998). 4.4. Peters, −2 −2 00 222 444 (mm) (mm) yyy(mm) 66 High Performance Performance Negative Negative Ions Ions Sources Sources Network, Network, 5.5. High Sources Network, HPRI-CT2001-50021, Supported Supported by by European European HPRI-CT2001-50021, by European community(2001). (2001). community 88 Sidlow,R., R.,etetal., al,EPAC EPAC96, 96,THP084L, THP084L,(1996). (1996). 6.6. Sidlow, (1996). FIGURE4.4. 4.Ion Ionsource sourceemittances emittancesfrom from the theISIS ISISRFQ RFQ test test FIGURE Ion source emittances from the ISIS RFQ test FIGURE stand. stand. stand. Thomason, J.J. W. W. G. G. and and Sidlow, Sidlow, R., R., EPAC EPAC 2000, 2000, 7.7. Thomason, R., EPAC 2000, THP4A07,(2000). (2000). THP4A07, Thesource sourceisisisvery verycompact, compact,and andthe theprimary primaryproblem problem The source very compact, and the primary problem The to solve is that of stabilisation of the cathode and solve isis that that of of stabilisation stabilisation of of the the cathode cathode and and toto solve anode temperatures at the higher power levels required anodetemperatures temperaturesatatthe thehigher higher power power levels levels required required anode forthe shortand andlong longpulse pulseoptions options by bymeans means of of for theESS ESSshort short and long pulse options by means of for controlled cooling. The thermal properties of the controlled cooling. The thermal properties of the controlled cooling. The thermal properties of the standard ISIS ISIS source source will will be be modelled modelled and and this this standard ISIS source will be modelled and this standard simulationwill willthen thenbe beextended extendedto tolonger longerduty dutycycles cycles simulation will then be extended to longer duty cycles simulation in order order toto to establish establish how how additional additional cooling cooling can can be be order establish how additional cooling can be inin 8. Thomason, Thomason,J.J.W. W.G., G.,etetal., al,RSI RSI73(2), 73(2),(2002). (2002). 8. 8. (2002). Smith,H. H.V., V.,etetal., al.,RSI RSI65(1), 65(1),(1994). (1994). 9.9. Smith, 10. Bailey, Bailey,C. C.P., P.,etetal., al.,EPAC EPAC2000, 2000,THP4A03, THP4A03,(2000). (2000). 10. THP4A03, (2000). 295
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