A prototype rf power source based on the Relativistic Klystron Two- Beam Accelerator (RK-TBA) concept is being constructed at LBNL to study physics, engineering, and costing issues. The prototype, called RTA, is described and compared to a full scale design appropriate for driving the Next Linear Collider. Specific details of the induction core test and pulsed power system are presented. Details of the 1-MeV, 1.2-kA induction gun currently under construction are described

Anderson, D.

Houck, T.L.

Westenskow, G.A.

UNT Digital Library

d Relativistic Klystron Two-Beam Accelerator Studies at the RTA Test Facility G.A. Westenskow, D. Anderson,i S. Eylon,? E. Henestroza,$ T.L. Houck, J.S. Kim,% S.M. Lidia,? L.L. Reginato,? D.L. Vanecek,? and S.S. Yu? $Lawrence Berkeley National Laboratory $University of California, Davis %Fusion and Accelerator Research This paper was prepared for submittal to the conference proceedings of the XVm International Linac Conference Geneva, Switzerland August 26-30,1996 August 16, 1996 I . .  . .  \ .;,. . ... U DISCLAIMER Thisdocumartwaspreparedasanaccountofworksporwredbyanagencyof the United States Government. 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RELATIVISTIC KLYSTRON TWO-BEAM ACCELERATOR STUDIES AT THE RTA TEST FACILITY* Parameter RTA Pulse Duration Flat-top 200 n.9. Rise Time. 100 ns Current 1.2 kA *hopper Extraction Sec.(dc) 600 A Extraction S e c . Q  1.1 kA Beam Energy Injector 1 MeV Chopper 2.8 MeV Extraction 4.0 MeV BunchCcnpression 240" to 110" Beamiralsptmthe Extraction Section B e m n  Period l m  LatticePeIiod 20 cm PhaseAdvance 720 0.5 870 G o=upancy Pole Tip Field G.A. Westenskowf', D. Anderson, S. Eylon, E. Henesm&, T.L. Houckt, J.S. Kim#, S.M. Lidia, L.L. Reginato, DL. Vanecek, S.S. Yu Lawrence Berkeley National Laboratory, One Cyclotron Road, Berkeley, California 94720, USA f' Lawrence Livermore National Laboratory, P.O. Box 808, Livermore, California 94550, USA * Fusion and Accelerator Research, 3146 Bunche Ave., San Diego, CA 92122, USA 5 University of California, Davis, CA 95616, USA TBNLC 200 ns loo ns 1.2 kA 600A 1.1 kA lMeV . 2.5 MeV 10.0 MeV 240" to 70" 2 m  333 cm 600 0.48 812 G Abstract ~._ - - -~ Frequency Power/S tructure structures Output Spacinp A prototype rf power source based on the Relativistic Klystron Two-Beam Accelemtor (RK-TBA) concept is being constructed at the Lawrence Berkeley National Laboratory to study physics, engineering, and costing issues. The prototype, called the RTA, is descn'bed and compared to a full *scale design appropriate for driving the Next Linear Collider (NLC). Specific details of the induction core test and pulsed power system are presented. Details of the 1-MeV, 1.2-kA induction gun cmently under construction are described 11.4 GHi 11.4 GHz 180 M W  360 M w  sw &lw 3-cellTw l m  2 m  Introduction For several years a Lawrence Berkeley National Labomtory (LBNL) and Lawrence Livermore National Laboratory (LXN,.) collaboration has studiedrf power sources based on the RK-TBA concept [l]. This effort has included both experiments [2] and theoretical studies. A prehhary design study for a rf power source using the RK-TBA concept suitable for an rf power source upgrade of the NLC collider design WNLC) has been published PI. The design specifically addressed issues related to cost, efficiency, snd technical issues. For a 1.5-TeV center-of-& energy design, the rf power source is comprised of 76 subunits, each about 340 m in length with 150 exat ion structures generating 360 MW per structure. Estimated conversion efficiency of wall plug energy to rf energy for this source could be greatea than 40%. Theory and simulations showed acceptable drive beam stability through the relativistic klystron, and no insurmountable technological issues were uncovered. We have established the RTA test facility [4] at LBNL to verify the analysis used in the design study. The principle effort is constructing a rf power source prototype where all major components of the TBNLC rf power source will be tested. The different sections of the RTA are descn'bed in Table 1. Due to fiscal constraints, the RTA will have only 8 rf extraction structures. Table 2 is a comparison between the pertinent parameters for TBNLC and the RTA. The pulsed power system and induction cells in the extraction section will be similar for both machines, allowing a demonstration of the wall-plug power to drive beam power conversion efficiency and establishing a basis for costing of the components. *The work whs perform under the auspices of the U.S. Department of Energy by LLNL, under contract W-7405-ENG- 48, by LBNL under contract ACO3-76SFooo98, and by FAR under SBIR grant FGO3-96ER82179. Table 1. RTA Accelerator Sections Table 2 Comparison between RTA and the TBNLC. BeamDjameter I 8mm I 4 mm RE' Power I Puked Power System . .  Conversion of wall plug power into induction drive beam power is a significant factor in the rf power source efficiency. The efficiency of a TBA induction d e n t o r  depenas on several factors. Beam W r t  dynamics will determine the size of the beam pipe. The rf power requirement detennines the pulse duration, beam current, accelerating gradient, and repetition rate. Once these factors are established, the outer radius and material of &e core can be calculated .from: AV-At = AB-A-F where AV is cell voltage swing, A t  is pulse duration, A% is core flux swing, A is core cross section, and Fp is core material packing factor. The core volume increases nearly as the radius squared, so smaller, more efficient and lower cost induction cells can noimaUy b~ obtained by using higher Al3 materials and minimizing the inner radius. Microwave Conductjve I ce-c Insulator absorber \/I- * Fig. 2. A proposed RIGTBA induction cell design illustrating longitudinal core segmentation. Several core materials have been tested at the RTA Test Facility [5]. Two METGLAS@ alloys, 2605SC and 2714AS, have been selected for use in the RTA. The alloy 2605SC has aAl3 of -2.5 T with a core loss of - 2 kJ/m3 for a 400 ns pulse and 20 pm thick ribbon. The alloy 2714AS has a lower AEl,-l.l T, but a much lower axe loss of -150 J/m3 with 18 pm ribbon. The core tests are performed with the expected pulse shape and duration for accmte loss measurements. For our TBNLC geometxy, the low core loss 2714AS can achieve a conversion efficiency of wall plug power to drive beam power of 59%, a substantial improvement over 2605SC. 10 : I 10 dB/dt V/w) 1 Fig. 3. Core loss for different rates of magnetic flux change. The modest repetition rate (120 Hz) and current rise time (100 ns) envisioned for the NLC permit the use of a simple, and cost effective thyrawn driven modulator. The total - .  'induction cell core is segmented longitudinally into smaller cores each individually driven at 20 kV or less. Driving at this voltage level avoids a separate step-up transformer and allows for switching with fast inexpensive Singlegap tubes. Length of the induction cell, thus number of cores per cell, is set by geometrical constraints due to extraction structures, magnet positions, etc. The TBNLC design in Fig. 2 has five cores per cell while theRTA has three cores. Beam energy flatness is an important issue affecting beam traac;port and rf phase variation. The current requkd to drive the cores is .nonlinear for a constant amplitude voltage pulse since the inductance of the core decreases as saturafiion of the material is approached. The effect is more pronounced for high aspect ratio (Ad&) cores due to non-unhm saturation starting at the inner radius propagating outward. This effect is shown in Fig. 4 where the voltage pulse has -200 ns of flat top during which the drive Current increases non-linearly. The genemted voltage amplitude can be kept constant, within bounds, as the material approaches saturation by tapering the impedance of the PFN stages. Our PFN will consist of many coupled L-C stages. We have been testing pulsed power prototypes using a 3 a r e  injector cells. In the prototype we have used EEV CX1538 and W O N  F-232 thyratron tubes. The injector cell design calls for 14 kV/core or 40 kV/cell. Early test performed using CX1538 tube did not yeild rise times below 100 ns, however a pretrigger applied to an additional grid on the tube gave performance (see Fig. 4) close to the design (100 ns rise time, 200 ns flat-top). The F-232 tube has lower internal inductance as well as a higher Wdt rating. It also gave performance close to the design criteria. 200 n s 100 5 5 V 0 0 0 200 ' 400 CX1538 Time (ns) Fig. 4. Injector cell voltage and current driven by a prototype pulsed power unit. The V,hgle trace shows the voltage waveform with a single trigger. The rise time (10% to 90%) was .about 150 ns with a voltage flat top of 120 ns. With a pretrigger to an additional grid on the tube we were able to get the rise time to down to 100 ns and obtain a voltage flat shows the PFN current for the dualirigger case.. top O f  180 IlS (Shown in vd,,d). The I d d  trace Injector The injector consists of two sections, a 1-MV, 1.2-kA induction electron source, xef& to as the gun, followed by several induction d e m o r  cells to boost the energy to 2.8 MeV. Two goals of the design are minimizing electrical field stress% in the gun and realizing the lowest possible emittance growth. Gun induction cores are segmentedradhlly to reduce the individual aspect ratios with each driven separately at about 14 kV. Components of the induction cells for the gun are in fabrication. Induction cores 12 induction cells with 3 cores/cell +9f3m-I Fig. 4. Schematic of the catlkde-half of the RTA electron gun. This section provides 05 MV of the guns potential. ' A novel feature of the gun design is the insulator, a single, 30 cm ID, PYREX@ tube with no intennedjate electrodes. Average gmdient along the insulator at the operating voltage of 500 kV is - 5.1 kV/cm. Maximum fields at the triple points, intersection of insulator, vacuum, and metal, are less than 3.5 kV/cm. Maximum. sut3c.e fields in thecathode half of the gun are about 85 kVfcm. Our design allows for the addition of intermediate electrodes an%r substitution of a ceramic insulator to offset the i n d  risk associated with this approach. The focusing solenoidal field profile must be optimized for the injector to control the beam radius while minimizing emittance growth. A new electrode pacbge and lagex dispenser cathode wil l  likely be required for the desired low emittance 1.2-kA, 1-MeV electron beam. The design goal is for beam radius less than 5 mm and horizontal normalized edge emittance less than 250 z-mm-mr at the end of the injector. Alignment of the solenoids is critical to avoid corkscrew motion and emittance growth. Incorporating homogenizer rings [q with the solenoids could reduce the need for correction coils and simpliy alignment. Experience operating other induction accelerators has shown that mefd alignment of the solenoids may not be sufficient to reduce the amplitude of the corkscrew motion to the 0.5 mm desired for the RTA injector. We plan to use a time independent steering algorithm developed at LLNL to control steering coils on the solenoids. The algorithm corrects for the Fourier component at the cyclotron wavelength of the field error. Beam Dynamics and RF Power Extraction Issues Beam dynamics issues related to longitudinal and transverse stability, modulation, and transport have been presented in detail elsewhere [3, 81. A brief description of these issues is given here. Initial beam modulation is accomplished with a transverse chopping technique. After this modulator section, an adiabatic compressor, a system of idler cavities and induction accelerator modules, is used to bunch the beam and further acceleaate it to an avemge energy of 4 MeV. ?he lowerfirequency component of the transverse beam breakup instability is controlled by Landau damping. Control of the higher m e n c y  component, excited in the rf cavities, is accomplished with the focusing system in a technique that we refa to as the "Betatron Node" scheme. The rf extraction structura are appropriately demed to compensate for space charge and energy spread effects so that the longitudinal current distribution is srable. After the adiabatic compressor, the beam enters the extraction section. where beam energy is periodically converted into rf energy (via extraction cavities) and mred to its initial value (via induction modules). Both traveling wave crw) and standing wave (SW) structures are being considered for the extraction section of the RTA. The TEINLC design 191 uses TW structures to reduce the surface fields associated with generating 360 MW per structure. RTA is designed to generate 180 M W  per structure. Thus, inductively detuned SW cavities are apractical alternative. ...- - c11 [41 References Sessler, AM. and Yu, S.S., Phys. Rev. Lett. 54, 889 (1987). Westenskow, G.A., and Houck, T.L., IEEE Trans. on Plasma Sci., 22,750 (1994). "An RF Power Source Upgrade to the NLC Based on the Relativistic-Klystron Tw@Beam-Accelerator Con- cept," Appendix A of the Zeroth-Order Design Report for the Next Linear Collider, SLAC Report 474, Stanford Unversity, Stanford, CA, May 1996. Houck, T.L., and Westenskow, G.A., "Prototype Microwave Source for a Relativistic Klystron Two- Beam Accelerate? to be published in IEEE Trans. on Plasma Sei., Special Issue on High Power Microwave Generators. Reginato, L., et al., ''Engineering Conceptual Design of the Relativistic Klystron Two-Beam Accelerator Based Power Source for 1-TeV NLC," Proc. 1995 IEEE Particle Accelerator Conf., p. 743. Feinberg, B., et al., Nucl. IMP. and Meth., 203, pp. 81-85 (1982). men, S.L., et al., 'Measurements of Reduced corksctew Motion on the ETA-II Linear Induction Accelerator," Proc. 1991 IEEE Particle Accelerator Con$, pp. 3094-3096. Proc. 1996 Pulsed RF Sources for Linear Colliders Workshop. Kim, J.S., et al., 'W Structure Design for the TBNLC," to be published in the 1996 Linac conference Pr==ws. HOUCk T.L., et A, 'RK-TBA prototype RF Source,'' 

Relativistic Klystron Two-Beam Accelerator studies at the RTA test facility

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Relativistic Klystron Two-Beam Accelerator studies at the RTA test facility

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