INITIAL RESULTS OF THE COMMISSIONING OF THE HRIBF RECOIL MASS SPECTROMETER

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INITIAL RESULTS OF THE COMMISSIONING OF THE HRIBF RECOIL MASS SPECTROMETER C. J. Gross Physics Division, Oak Ridge National Laboratory, Oak Ridge, TN 37831 and Oak Ridge Institute for Science and Education, Oak Ridge, TN 37831 Y. A. Akovali, M. J. Brinkman, J. Mas, J. W. McConneII, W. T. MiIner, Physics Division, Oak Ridge National Laboratov, Oak Ridge, TN 37831 T. N. Ginter Physics Department, Vanderbilt Universiy, Nashville, TN 3 7235 and Joint lnstitutefor H e w Ion Research, Oak Ridge, 17v 37831 A. N. James Department of Physics, University of Liverpool, Liverpool L69 3BX UK and Joint Institute for Heavy Ion Research, Oak Ridge, I1v 37831 The recoil mass spectrometer at the Holifield Radioactive Ion Beam Facility is currently undergoing commissioning tests. This new spectrometer is designed to transmit ions with rigidities of K = 1 resulting from fusion-evaporationreactions using inverse-kinematics. The device consists of two sections: a momentum separator to provide beam rejection and a mass separator for product identification. Using normal-kinematic and symmetric reactions, the commissioning tests have shown that the NQ acceptance is almost k 5%, the energy acceptance is approximately -t 12%, and there has been little, if any, primary beam observed on the focal plane. Commissioning tests are presently underway with reactions using inverse-kinematics. A recoil mass spectrometer (RMS) is currently undergoing commissioning tests at the Holifield Radioactive Ion Beam Facility (HRIBF). Similar devices, which are often used to identify exotic nuclei resulting from compound nuclear reactions, are located at many laboratories throughout the world [1-4]. The RMS at the HRIBF represents a new generation of spectrometers [5] by combining a momentum separator for primary beam rejection and a mass separator for product identification. A. COMPONENTS OF THE RMS A schematic of the K = 1 Rh4S is shown in Fig. 1 and has been described in-depth in Ref [5-71. In summary,it consists of three magnetic dipoles (D), seven quadrupoles (Q), two sextuples (S), and two electric dipoles (E). The physical properties of each element may be found in Ref. [5]. The fust two quadrupoles gather the recoiling nuclei and determine the momentum focus which is located inside 4 3. The fmt magnetic dipole separates the recoiling nuclei fiom the beam based on momentum. The primary beam, originating fiom a tandem accelerator, has a well-defined momentum and should be focused spacially according to its charge-state distribution. The recoils have a large momentum distribution caused by the evaporation process and will thus, fill the available space. Small rods called fingers may be inserted through the split poles Of 43 to intercept the primary beam at its focus and still have minimal impact on the overall transport efficiency for recoil products. These fingers are intended for use with inverse-kinematic reactions where beam particles and recoils have similar rigidities and hence, would all be accepted by the FWS, these fmgers could provide beam rejection factors of ioj3. The second half of the momentum separator, D2Q4Q5,provides a second focus which serves as the object for the mass separator portion of the spectrometer. This position, called the achromat, is energy independent when 43 is correctly adjusted. The two sextuples provide second-order corrections in the fmal focus. The mass separator section contains a magnetic dipole between two electric dipoles. The electric The submitted manuscript has been authored by a contractor of the U S. Government under contract No. DE-AC5-96R22464. Accordingly, the U.S. Government retains a nonexclusive, royalty-fiee license to publish or reproduce the published form of this contribution, or allow others to do so, for U.S. Government purposes. -~~ ~ ~ ~-

DISCLAIMER Portions of this document may be illegible in electronic image products. Images are produced from the best available original document.

DISCLAIMER This report was prepared as an account of work sponsored by an agency of the United States Government. Neither the United States Government nor any agency thereof, nor any of their employees, makes any warranty, exprtss or implied, or assumcs any legal liability or responsibility for the accuracy, completeness, or usefulness of any information, apparatus, product, or process disclosed, or represents that its use would not infringe privately owned rights. Reference herein to any specific commercial product, process, or service by trade name, trademark, manufacturer, or otherwise does not necessarily constitute or imply its endorsement, reammendation, or favoring by the United States Government or any agency thereof. The views and opinions of authors expressed herein do not necessarily state or reflect those of the United States Government or any agency thereof.

Achromatic Focus 21 i \ Momentum 11 Plane 82 31 - Turqet Position FIGURE 1 The layout of the RMS. The fingers are located at the momentum focal plane located inside Q3. elements separate the recoils as a function of kinetic energy and charge (E/Q) and the magnetic dipole separates as a function of momentum and charge (P/Q). The net result are recoils separated as a function of mass and charge (A/Q). The magnitude of the mass dispersion is determined by the last pair of quadrupoles, 4 6 and 47. Together with Q4 and Q5, the position of the final focal plane is determined. The performance parameters of the spectrometer, such as the size of the fmal image and the mass dispersion, often depend only upon specific groups d elements of the RMS. These elements may be adjusted together without affecting the field values of the other elements. Thus, several knobs have been incorporated into the control system so that users may adjust these parameters according to the requirements of the experiment. B. DESIGN PERFORMANCE PARAMETERS Various acceptances govern the performance of the RMS and its efficiency to detect recoil products. The RMS is a zero degree device and has an asymmetric, overall solid-angle acceptance. The horizontal acceptance is k 3 mrad and the vertical acceptance is k 115 mrad and is determined by the positions of Q1 and 42. The target-to-q1 distance is 75 cm. However, other apertures in the system affect the effective overall solid angle which ranges between 1- and I5 msr. The primary beam spot on target should be a vertical line.5 mm in width and 2 mm in length. The energy acceptance is determined, in part, by the length of the plates of the electric dipoles and is estimated to be some f 15% at the base. The A/Q acceptance, reflecting the various apertures throughout the Overall mass resolution flight path is near k 5%. (WAM) has been calculated to be 54 although through collimation, it is estimated that this value may approach 1 (including software corrections). C. COMMISSIONING DETECTORS The mainstay detector of the RMS is the positionsensitive avalanche counter (PSAC) located at the final focal plane ofthe RMS. This detector has an active area of 36 cm by 1 cm and is filled with isobutane gas. The arrangement of planes with respect to the beam is cathode, horizontal sensing plane (electrically split in half), anode, and vertical sensing plane. The anode and cathode have 2 p n gold-plated tungsten wires spaced 1 mm apart. The position sensing planes have the same wires which are spaced 2 mm apart and are connected to delay-lines using 2 ns taps per wire. The overall position resolution attainable with this device is approximately 2 mm. The total PSAC efficiency (defined as those events which cause an anode signal) is better than 9%. Behind the focal plane, several detector systems may be used. Double-sided silicon-strip detectors (see contribution by K. S. Toth, et a,.), an ionization chamber, and a moving tape collector have been constructed and will undergo commissioning tests this year. At the target position, a germanium detector array consisting of segmented-clover detectors (4 Ge detectors in a single housing) and conventional Ge detectors will be used. In the present tests, only four conventional Ge detectors have been used in conjunction with the PSAC to confirm mass identification.

D. INITIAL PERFORMANCE An alpha source and four reactions have been used to commission the Rh4S and these are listed in Table 1. reaction products using double-sided silicon-strip detectors. See the contributionto these proceedings by K. S. Toth, et af. for information about these tests. The highest mass resolution achieved so f b has been M / M = 45 using the Ni+Ni reaction and is shown in Fig. 2. The energy acceptance of the spectrometer has been measured to be at least +- 12.5%. This value is smaller than similar devices (& 2%) due to the longer plates of the electrostatic dipoles. The A/Q acceptance has been measured to be in excess of 4.5%. A total reaction efficiency has been estimated to be 1-2%. Because this efficiency is for all fhsion-evaporation recoils, individual channel efficiency will vary with pure nucleon evaporation channels being more efficient than alpha evaporation channels, These efficiencies will increase when inverse-kinematic reactions are used. One persistent feature of the commissioning tests so far, has been the absence of beam on the focal plane. The momentum separator is clearly preventing scattered beam from reaching the PSAC allowing high primary beam 116 114 172 494 227 15 48 m Ip 22s 1 P 5s 2 5: 1 " 5+ 112 115 M / b = 45 FIGURE 2 The focal plane image resulting from the reaction Ni+Ni reaction. The mass resolution WAM = 45. The spectrum was generated from the PSAC requiring that the sum of each delay-line signal falls within a relatively small gate and the entire range is shown. This spectrum has no other gating conditions. Notice the absence of beam in this spectrum.

15 - r: f a c A=87 75 Q) \ u) currents to be used. Most tests have been conducted with 15 pna, or more, yet the PSAC has always run at less than 1 khz. Mass 86 and 87 y ray spectra are shown in Fig. 3. These data were taken with the S+Ni reaction and demonstrate the channel selection sensitivity of the RMS. Only those known transitions in %b, 86Zr, and * Nb can be observed in their respective mass-gated spectrum. Further commissioning tests will be continuing throughout this year and in 1997. Inverse-kinematic reactions and the successlkl use of the finger system will constitute a large portion of our future efforts. Our upgraded Ge array will become available in 1997, as well as, a 4n charged particle ball located at the target position. Neutron detectors will also augment this inbeam spectroscopy system. The ionization chamber and tape collector plus pair spectrometer plus Clover Ge system will also be tested in the coming months. As radioactive ion beams become available for nuclear structure studies, the RMS stands ready to investigate nuclei far from stability, E. ACKNOWLEDGMENTS We would like to acknowledge the work perfonned by P. F. Mantica, J. J. Das, and R. L. Auble on the installation of the RMS. One of us (J. Mas) acknowledges support f?om the SERS program administered by Oak Ridge Associated Universities. Research sponsored by the Oak Ridge National Laboratory, managed by Lockheed Martin Energy Research Corporation for the U.S. Department of Energy under contract number DE-AC5-96R22464. This work was also supported by the U.S. DOE under contract number DE-AC5-76R33 (Oak Ridge Institute for Science and Education). ci C $15 F. REFERENCES 75 75 Channel Number FLGURE 3 Mass 86 and 87 gated y ray spectra from the S-tNi reaction. [l] Cormier, T. M., et ai., Nucl. Instrum. Methods 212, 185 (1983). [2] James, A. N., et al., Nucl. Instrum. Methods in Phys. Res. A267, 144 (1 988). [3] Spolaore, S., et af., Nucl. Instrum. Methods A238, 381 (1985). [4] Davids, C. N., et al., Nucl. Instrum. Methods in Phys. Res. B7, 358 (1992). [5] Cole, J. D., et ai., Nucl. Instrum. Methods in Phys. Res. B7, 343 (1992). [6] Cole, J. D., et ai., in Exotic Nuclear Spectroscopy, edited by C. McHarris, (Plenum Press, New York, 199), p 11. [7] Mantica, P. F., Nucl. Instrum. Methods in Phys. Res. B99, 338 (1995).