Nuclear Instruments and Methods in Physics Research A 503 (2003) 336–339 Experimental observation of proton-induced shocks and magneto-fluid-dynamics in liquid metal A. Fabich*, J. Lettry CERN, CH-1211 Geneva 23, Switzerland Abstract A liquid metal target is one of the options for the pion production target of a n-factory. The interaction between a liquid metal and a proton beam were observed with static mercury as well as with a free mercury jet and up to 4 1012 protons/bunch. The experimental method for investigating the magneto-fluid-dynamic effects of a high-velocity liquid metal in a high magnetic field magnet has been validated by recording the behaviour of a 15 m=s mercury burst entering the gradient of a 13 T solenoid at GHMFL Grenoble. The paper includes the description of the optical read-out system as well as numerical results of the mercury drop velocities. r 2003 Elsevier Science B.V. All rights reserved. PACS: 47.65.+a; 29.25.Pj Keywords: Target; High power; Mercury; MFD; Neutrino factory 1. Introduction The liquid metal target is a natural solution to the stresses and fatigue, induced by the proton beam, that eventually lead to the destruction of most solid targets. A liquid jet would provide a new target for each proton pulse if the material disrupted by the proton beam can be evacuated within the proton pulse interval. To study the interaction of a liquid metal with a proton beam a static mercury target and a mercury jet with free surface have been exposed to a proton beam ð24 GeV; 150 ns) at the AGS, BNL (experiment E951). Mercury was chosen as one of the room*Corresponding author. E-mail address: [email protected] (A. Fabich). temperature liquid metals. Its high density reduces the physical length of the target and influences the design of the pion capture system, the spread in time of the resulting p-burst, and the absolute pion production [1]. For the pion capture system, in the environment of the target, two scenarios are proposed. The CERN community is presently going for a magnetic horn scheme. The US scenario includes a 20 T solenoid with injection of liquid metal into a high magnetic field. The experimental setups are based on the recording of the shadow of the mercury, intercepting a laser light source, with a high-speed camera. Sets of mirrors and telescopes allow the installation of the sensitive pieces of electronics out of the magnetic field or behind a few meters-thick radiation shielding. 0168-9002/03/$ - see front matter r 2003 Elsevier Science B.V. All rights reserved. doi:10.1016/S0168-9002(03)00710-1 A. Fabich, J. Lettry / Nuclear Instruments and Methods in Physics Research A 503 (2003) 336–339 2. Interaction of the mercury target with a proton beam 2.1. Experimental setup Thimble: The thimble experiment provides a simple setup to study the phenomena at proton impact on liquid targets. The amount of mercury, which is irradiated, is by far smaller, as no spare material for circulation is needed. As experiments for both setups under the same conditions were performed, the results can be compared against each other, and future experiments with a thimble can bring up results which can be scaled to the case of a free jet target. The volume of the thimble excavated in a stainless-steel frame is 1:2 cm3 : It consists from bottom to top of a half-sphere ðr ¼ 6 mmÞ; a vertical cylinder ðr ¼ h ¼ 6 mmÞ; and a meniscus, which has a free surface of 1:2 cm2 : Jet: The continuous jet was ejected from a cylindrical nozzle (diameter 1 cm) under an angle of 14:5 from the horizontal plane and followed by a parabolic line. The view of the camera, which covered a round area with a diameter of about 8 cm; was centred on the zenith of the jet. With the beam centre line at the zenith of the jet a total physical intersection of jet and beam is given along a distance of 19 cm: In total, 12 proton pulse impacts on jet and target have been performed. The main parameter of the beam is the proton intensity, which was varied from 1–4 TP:1 The effects of the parameters ‘beam spot size’ and ‘bunch length’ cannot be determined due to low statistics. The information of the spot size was measured with an alumina foil ðrr:m:s: ¼ 1:5 mm 1 mm; horizontal/vertical). Measured quantities as a function of the proton intensity per pulse are the explosion velocity and disruption length and offset. The disruption length and its offset relative to the zenith are only measurable in the jet setup, as there is no equivalent in the case of the thimble. Temperature profile: The temperature distribution within the target has been simulated for the two experiments using MARS [2]. Assuming a proton pulse with an intensity of 4 TP and a spot 1 1 TP ¼ 1012 protons: 337 size radius of 1 mm (r.m.s.) the main characteristics are an average temperature rise in the target centre of 200 K for the thimble and 300 K for the jet target. The radial distribution is a parabolic slope down to Zero at the boundary of the target. The average temperature rise is 57 K (thimble) and 65 K (jet). The two temperature distributions are very similar, in the case of the jet the shower is more developed as the target length ðl ¼ 19 cmÞ is about 1.5 interaction lengths. 2.2. Velocity measurements The velocities measured from the movies of the thimble and jet splashes are plotted in Fig. 1. The data points represent drop sizes greater than 1 mm as a result of our resolution. A small fraction of the jet is dispersed into small, fast droplets. The larger part ðE80%Þ is not accelerated that high. The upper limit of the dominating velocity is indicated by the solid line. The errors of the shutter time ðt ¼ 25 msÞ and the spatial resolution ð0:89 mm=pixelÞ result in an error of the velocity measurement of 5%. Fig. 1. Droplet velocities measured over a typical distance of 2 cm for the thimble (triangle) and the jet (circles). The solid line shows the upper limit of the dominating velocities (jet). Also indicated is the theoretical velocity according to Ref. [3] for the jet (dashed line). The theoretical velocity for the thimble is about 30% below the one of the jet due to the lower temperature rise. 338 A. Fabich, J. Lettry / Nuclear Instruments and Methods in Physics Research A 503 (2003) 336–339 Assuming the model given in Ref. [3], the explosion velocity v is estimated as the ratio of thermal expansion by the time the sound wave needs to travel to the boundary of the mercury target and is given by v ¼ 0:25aV DT0 c; where aV is the volume expansion coefficient, DT0 the temperature rise on the centre axis, and c the velocity of sound in the medium. These predicted velocities for the jet are indicated in Fig. 1 and agree nicely with the measurements. 2.3. Disruption length of the jet An interesting number, to decide between a pulsed or continuous jet as a target, is the length for which the jet is disrupted. As the jet passes the viewing area of the camera, the extension of the destructive interaction between the p-beam and the mercury jet can be determined by computing the origin of the Hg drops. From this it can be learned whether a destructive pressure wave is travelling along the mercury jet outside the initial geometrical intersection region. Fig. 2 is a scattered plot of the disruption length and position as a function of the distance along the jet and the proton intensity. Fig. 3 shows a projection of Fig. 2 on the position axis, where the ordinate shows the number of entries, which is proportional Fig. 2. Disruption length and its position along the jet for all eight pulses at different proton intensities. The dashed line indicates the invisible disruption for the event at 3:8 TP; where the disruption is extended to outside the viewing area. Fig. 3. Probability of jet rupture and its Gaussian fit. The two bars indicate the viewing length of the jet (black) and the physical intersection region of jet and beam (pattern). For an 4 TP-proton impact the temperature rise on axis along the jet is shown (dashed). Proton beam and mercury-jet ðv ¼ 2:5 m=sÞ arrive from the right. to the probability of rupture of the jet. We observed no rupture outside the geometrical intersection region and therefore support a continuous jet target option. 3. Magneto-Fluid Dynamics A magnetic horn [4] and a 20 T solenoid [1] are proposed for the pion capture system for Neutrino factories. Using a mercury jet as a target, a liquid metal is injected into a magnetic field and magneto-fluid-dynamic (MFD) effects occur. In spring 2001 an experimental setup has been tested at the Grenoble High Magnetic Field Laboratory (GHMFL). A mercury jet of a diameter of d ¼ 3 mm has been injected into vertical solenoid ðBmax ¼ 13 T; ð@B=@zÞmax ¼ 65 T=m; dbore ¼ 12 cmÞ with a velocity of up to v ¼ 15 m=s: On injecting a mercury jet into a magnetic field, a repulsive force acted on the tip of the mercury jet. This resulted in a shaping of the mercury tip towards a shape similar to the tip of a rocket. The MFD effects observed during the on-axis injection were qualitatively predicted [5] and confirmed the sensitivity of the measurements. A. Fabich, J. Lettry / Nuclear Instruments and Methods in Physics Research A 503 (2003) 336–339 4. Conclusion * * * * The mercury thimble and jet experiments confirmed reasonably the predictions for the behaviour of a liquid metal target at the impact of a proton pulse. The thimble provides a simple setup for studying proton-induced shocks. Dominating velocities measured were up to 10 m=s and the maximum velocity of up to 45 m=s for a bunch intensity of 4 1012 protons. The rupture of the mercury jet outside the intersection of jet and beam did not occur, which makes the use of pulsed target jets unnecessary. The MFD measurement setup is validated and showed quantitatively the expected effects. Acknowledgements We would like to thank our colleagues from the E951 collaboration at BNL, the CERN horn and targetry group and the staff of GHMFL in Grenoble for their great support. 339 References [1] N. Mokhov, p=m Yield and power dissipation for carbon and mercury targets in 20-Tesla solenoid with matching section, MUCOLL Note 61, BNL 1999. [2] N.V. Mokhov, The Mars Code System User’s Guide, Fermilab-FN-628, 1995; N.V. Mokhov, MARS Code Developments, Benchmarking and Applications, Fermilab-Conf-00-066, 2000; N.V. Mokhov, S.I. Striganov, A. Van Ginneken, S.G. Mashnik, A.J. Sierk, J. Ranft, MARS Code Developments, Fermilab-Conf-98/379, 1998; N.V. Mokhov, S.I. Striganov, A. Van Ginneken, S.G. Mashnik, A.J. Sierk, J. Ranft, LANL Report LA-UR-985716, 1998; N.V. Mokhov, S.I. Striganov, A. Van Ginneken, S.G. Mashnik, A.J. Sierk, J. Ranft, nucl-th/9812038, Vol. 2, 16 December 1998; O.E. Krivosheev, N.V. Mokhov, A New MARS and its Applications, Fermilab-Conf-98/43, 1998. [3] P. Sievers, P. Pugnat, Response of solid and liquid targets to high power proton beams for neutrino factories, CERNLHC/2000-4 (CERN-NuFACT Note 035), 2000 [4] A. Ball, et al., Preliminary magnetic horn studies in the collection scheme for a neutrino factory, in: Proceedings of the NuFact 99, Nucl. Instrum. and Meth. 451 (2000) 359–361. [5] P. Thieberger, Estimated perturbations of the axial motion of a liquid-metal jet entering a strong magnetic field, MUCOLL Note 182, BNL 2000.
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