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© 1977 IEEE. Personal use of this material is permitted. However, permission to reprint/republish this material for advertising or promotional purposes or for creating new collective works for resale or redistribution to servers or lists, or to reuse any copyrighted component of this work in other works must be obtained from the IEEE. TEE T&rn.&actionb A 100-mA Institute of Nuclear NEGATIVE G. I. Dimov, Physics, Siberian on Mu~eah Science, HYDROGEN-ION Vo.!..NS-24, SOURCE No.3, June 1977 FOR ACCELERATORS G. Ye. Dereviankin, and V. G. Dudnikov Division, USSR Academy of Sciences, Novosibirsk In the Institute of Nuclear Physics of the USSR Academy of Science a surface-plasma source of Hions has been developed, designed for powerful linear accelerators (meson factories) and also for circular accelerators with charge-exchange injection of protons, especially for boosters of the proton synchrotrons. Parameters of the source (nominal values are given in parentheses) are: repetition rate of up to 100 (100) Hz, current pulse duration of 100-300 (ZOO) msec , output current of the H- ion beam of up to 150 (100) mA, ion energy of IO-30 (20) keV. The source, as is shown in Fig. 1, is mounted on a metal flange (1) of the forinjector accelerating tube (2) inside a cylindrical shield (3). The magnet yoke (5) is suspended to the flange on a bar (4). The magnet is excited by the water-cooled coils placed in vacuum-tight metal housings (6). The magnet is the most massive part (40 kG). A gas-discharge chamber (7) which is fixed on the magnet with high-voltage A insulators (8) is a direct source of the H- ions. negative-ion beam is extracted through the emission slit of the gas-discharge chamber with electrodes (9) The gas-discharge chamber installed on the magnet. is under the negative potential of up to 30 kV. The beam of H- ions passes between magnet poles (10) where it is turned at 90’ by the magnetic field and injected through holes in the yoke (5) and the shield(3) into the first accelerating gap of the tube (2). The mean radius of the ion trajectory in the magnetic field is 7 cm. A gap between the poles on this radius is field with the 3 cm. The poles form the magnetic radial droop index n = 1. By virtue of this, together with the beam separation in this field an onedimensional focusing of a beam in the plane parallel to for such the field is carried out. The necessity focusing is connected with a large divergence of the In the plane beam in an extraction gap in this plane. perpendicular to the field the beam divergence is At the accelerating tube input the ion close to zero. beam has a nearly round cross section of about l-cm At the sides of the poles (10) the small diameter. rectangular pole pieces are installed to form the magThe nominal netic field in the gas-discharge region. bending magnetic field on the mean ion trajectory is 2.9 kG, and about 1 kG in the gas-discharge chamber The gas-discharge chamber (7) is assembled region. together with small pole pieces and extracting electrodes (9) and installed, as a unit, on poles (10). The gas-discharge chamber feeding with hydrogen, cooling air, water, and voltage is performed through a parThe beam current tition insulator in the flange (12). control at the source output is performed by the Rogovsky coil ( 11). It is assumed that the hydrogen from the source will be pumped out through the holes in a cylindrical shield (3) and thrn through an accelThe mean hydrogen pressure inside the erating tube. shield should be maintained at the level of 10m4 Torr. At this pressure the necessary hydrogen pumping speed is up to 2000 l/set. 90, USSR The source of H- ions has been described earlier in Ref. 1. To increase the source lifetime and make better ion-optic characteristics of a beam, the source ’ design has, to a considerable ‘extent, been improved. The improved design of the gas-discharge chamber with extracting electrodes is presented in Fig. 2. The Penning type gas-discharge cell is mounted in a chamber body (1) to which the wall with the emission slit (2) is welded. An anode insert (3) embracing molybdenium cathode (4) is placed into the chamber body. There is a slot, in the cathode, parallel to the emission slit, 15 mm long and 5 mm wide. The anode insert crosspiece of 4 mm wide passes through this slot near its bottom. A lower free part of’the slot, adjacent to the emission chamber wall, 2.7 mm deep, is is a gas-discharge region. Its volume is 2.7X 5 X 15 mm3. The active surface area of each cathode formed by the opposite walls of the slot is 2.7x 15 mm2. The magnetic field formed by poles ( 10) and lugs (11) is directed normally to the active cathode surfaces, and in the extracting gap it is concave toward the emission The emission slit in the chamber wall (2) is perslit. pendicular to the magnetic field; it has the dimensions of 0.5mmx 10mm (the thickness of its edges is 1 mm). In the wall (2) behind the emission slit, the anode groove is made of 1 mm deep. cell has been The geometry of the gas-discharge chosen according to the concepts of the surfaceplasma source operation principles2 taking into account conditions for the discharge ignition and burning as well as the work duration. The H- ions producing on electrodes due to the secondary emission and the reflection of hydrogen particles come to the anode groove at a relatively high energy. As a result of charge exchange of these ions with atomic hydrogen, slow negative ions are produced in the anode groove. Then slow negative ions come through the emission slit to the extraction gap. Both direction and divergence of the beam being extracted in the plane parallel to the magnetic field, are sensitive to the extraction-gap geometry. To maintain the beam geometry invariable a very fast fixation of extracting electrodes (13) and the emission wall of the gas-discharge chamber (2) are necessary as well as the limitations for their distortions due to gap is The geometry of the extraction heating. accepted to be similar to the Pirs geometry; the extraction gap length is 1.5 mm, the gap between extracting electrodes is 0.8 mm. In the nominal regime the mean power of the gasdischarge is 250-300 W. According to the measurements3 70-75s of this power is released on the cathode. The cathode is cooled with the cooler (5) which has a thermal contact with the cathode and through which the The cathode temperature is mainwater is passed. tained at the level of 600’ C. The anode is cooled with wall air passed through channels (14) in the emission 1545 With the hydrogen density increase in the discharge and the magnetic field decrease, the random fluctuations are first converted into harmonic oscillations with frequences of 17-18 mHz and decreased then below the recorded level. The hydrogen density in the discharge chamber necessary for the noiseless regime is about 1.5 times higher than that required for the discharge ignition. of the chamber (2). The temperature of this wall is maintained at the level of $00’ C, and together with the limitation for its thermal expansion, provides optimum covering of cathode surfaces by cesium and also limits the Cs-vapor yield through the emission slit within time intervals between the gas-discharge pulses. Cesium is led in the gas-discharge region along the channel in the anode, through the metal wick from the preheated container with cesium (17). The cesium consumption is 0.1 g per 100 hours of the source operation. The hydrogen is led through channels of the anode insert crosspiece in the gap between the The gas efficiency of the crosspiece and cathode. source is rather high due to separation of the hydrogen inlet from the emission slit by the gas-discharge region in which the hydrogen molecules are efficiently ionized by electrons. The hydrogen filling is performed in 200 msec pulses with an electromagnetic valve4 at a large work resource (more than 109 switchings). The hydrogen consumption is mostly determined by a volume of the gas-discharge cell and by a hydrogen density necessary for the discharge ignition and pulse frequency. The hydrogen consumption is about 1 cm3 Torr per impulse. The source and extraction voltage is provided by the pulsed electric power supply. Voltages on the discharge and extraction gap as well as corresponding currents are presented by oscillograms in Fig. 3. The discharge voltage is close to 100 V, the discharge current in the nominal regime is 100-120 A. The extraction circuit current is 200-200 mA. The reduced microperviance of the nagative-ion beam with nominal parameters is quite high, about 1.5. This means that for the beam transportation either a very strong focusing or compensation of the negative space charge in a beam with positive ions is Accumulation of positive ions in the beam required. due to the residual gas ionization is accompanied with elimination of some fraction of negative ions in the Therefore, with the compensation time beam. decrease due to the residual gas-density increase, the beam attenuation becomes higher. At the residual gas pressure of 5x 10-5 Torr, the observed compensation time of the beam is several tens of microseconds: the output current of negative ions in the beam (25 cm from the emission slit) is 90-950/o of the total current With the pressure increase of the extracted H- ions. up to 10m4 Torr, the compensation time decreases respectively, and the output current is reduced down to 80% of the total current of the extracted H- ions. If the low-frequency fluctuations are available in the discharge and the residual gas pressure around the beam is several times lower than 10-4 Torr, the negative-ion beam diameter at the output increases up to 3.5 cm, and its normalized emittance reaches the value of 4X 10-5 cm rad X 2 X 10-4 cm rad (the first number concerns the direction parallel to the magnetic field, the second the perpendicular direction). With the residual gas pressure increase up to the value of iOv4 Torr, the beam emittance decreases 1.5-Z times for each of the directions, At the noiseless region of the discharge the measured normalized beam emittance at the output is equal to 3 X 10-6 cm rad X 2 X 10w5 cm rad5 at nominal parameters. The current distribution in the output beam cross section is given in Fig. 4 where it is seen that the beam diameter is close to 1 cm. The total angular spread of H- ions at the output is iOv3 rad along the magnetic field and 10m2 rad across the field. The transverse energies on the emission surface are - 8 and -2 eV, respectively. The observed dependence of the phase volume of a negative ion beam on the noises in the discharge and the gas density around the beam is connected with emission surface fluctuations and spreading the ions in the angles on undercompensated and overcompensated domains of the beam which are formed due to the fluctuations of its intensity. The arise of instability of a compensated beam is also possible. Resource tests of the source have shown that the erosion of the gas-discharge chamber components does not lead to significant change in its parameters during 300 hours of continuous work. References A phase volume of the output beam considerably depends on the level and kind of noises in the gasdischarge as well as on the gas density in the beam region. This discharge in hydrogen with Csadmixture at the lower hydrogen density and higher strength of the magnetic field is characterized by the random fluctuations of volta e and discharge current The fluctuation level with frequencies of i05- 10BHz. ln this case, the may be of several tens per cent. beam intensity of the extracted H- ions fluctuates too. 1546 i. V. G. Dudnikov, Trudy 4-go Vsesoyuznogo soveshchania po uskoriteliam zariazhennykh chastits, Moscow, 1975, tom I, p. 323. 2. Y. I. Bel’chenko, V. G. Dudnikov, 68 (1975). G. I. Dimov, and Zhurnal Tekhnicheskoi Fiziki 45, 3. Y. I. Bel’chenko and V. G. Dudnikov, IV Vsesoyusnaia konferentsia po vzaimodeystviyu atomnykh chastits s tverdym telom, Khar’kov, 1976, chast’ 3, 180. 4. G. Ye. Dereviankin, V. G. Dudnikov, and P. A. Zhuravlev, Pribory i tekhnika eksperimenta, 1975, N 5, 168. 5. G. Ye. Dereviankin, V. G. Dudnikov, and V. S. Klenov, Preprint IJaF, 77-8, Novosibirsk, 1977. I 0 I L I I 5 to I d -t-\. :*I, ii_.-.-.. t.ti-T_. i-m- L 20 GM Fig. 1. Source Design. 1 - high-voltage flange of accelerating tube; 2 - accelerating tube; 3 - source shield; 4 - supported bar; 5 - magnet yoke; 6 - magnet coils; 7 - gas-discharge chamber; 8 - highvoltage insulators; 9 - extracting electrodes; 10 bending magnet poles ; 11 - Rogovsky coil; 12 partition insulator. ‘I- Fig. Oscillograms: Up - voltage on gas-discharge current; U, - extracting voltage; - discharge I - &rent in the extraction circuit; I- - current in I?- beam at the source output. gap; I_-_LL--. r I 2 J 3. I 1c. Source. 1 - gasFig. 2. Design of Negative-Ion discharge chamber body; 2 - emission wall of chamber; 3 - anode insert; 4 - cathode; 5 - Cooler of cathode; 6 - cathode insulator; 7 - high-voltage insulators; 8 - corbel-pieces embracing insulators; 9 shields of insulators; 10 - magnetic pole pieces; 11 lugs of poles; 12 - base piece; 13 - extracting electrodes; 14 - channels for cooling anode; 15 - tubes for cooling anode; 16 - tubes for cooling cathode; 17 - cesium feeder; 18 - hydrogen valve; 19 - hydrogen inlet pipe; 20 - tubes for cooling valve. -45 0 UC5 XCM -0.5 10.5 f” 1 in the Fig. 4. The negative ion current distribution output beam cross section. On the left - distribution along the direction parallel to the magnetic field. On along the direction perpendicthe right - distribution ular to the magnetic field. 1547