CP620, Shock Compression of Condensed Matter - 2001 edited by M. D. Furnish, N. N. Thadhani, and Y. Horie © 2002 American Institute of Physics 0-7354-0068-7/02/$ 19.00 ADVANCED CRYOGENIC SYSTEM CAPABILITIES FOR PRECISION SHOCK PHYSICS MEASUREMENTS ON Z D. L. Hanson, R. R. Johnston, M. D. Knudson, J. R. Asay, C. A. Hall, J. E. Bailey, and R. J. Hickman Sandia National Laboratories, Albuquerque, NM 87185 USA Abstract. We have developed a general purpose cryogenic target system for precision EOS studies with the Sandia Z accelerator short-circuit current drive. Condensation of large-area cryogenic liquid samples is accomplished using a cryostat evaporation refrigerator, shielded for survivability in the Z blast environment and connected by a thermal link to an expendable sample holder with active temperature control. Accurate shock physics measurements are performed using multiple, thermally isolated, fiber-optic-coupled VISAR interferometry, active shock breakout, and time-resolved optical spectroscopy diagnostics. We describe variations of this cryogenic system currently under development for three EOS measurement applications: (1) liquid D2 shock Hugoniot experiments using magnetically driven flyer plates; (2) liquid N2 isentropic compression experiments; and (3) EOS measurements on liquid 4He at 1.5 K. INTRODUCTION N2, O2, and Ar. In this paper, we will describe variations of this cryogenic system currently under development for three EOS measurement applications on Z: (1) liquid deuterium (LD2) shock Hugoniot experiments using magnetically driven flyer plates; (2) liquid nitrogen (LN2) isentropic compression experiments; and (3) liquid 4He (LHe) EOS measurements. Recently we have used the fast pulsed power technology of the Sandia Z accelerator (20 MA peak current in the long-pulse, short-circuit mode) to develop new experimental techniques for accurate EOS measurements at high pressure. Magnetic pressure loading of material samples in high current density electrode geometries on Z allows the generation of continuous isentropic compression curves previously unavailable at Mbar pressures [1] and the launching of magnetically driven flyer plates at velocities exceeding 20 km/s for accurate shock Hugoniot measurements [2]. To extend the range of materials that may be studied using these new precision EOS techniques, we are developing a general purpose cryogenic target system for Z. Cryogenic samples are cooled with a cryostat evaporation refrigerator, shielded for survivability in the Z blast environment. The version of the system currently in use is capable of condensing large area cryogenic liquid samples from a variety of permanent gases with normal boiling points above 15 K, including H2, D2, Ne, LD2 HUGONIOT MEASUREMENTS We have recently performed Hugoniot measurements of LD2 in the range of 25-70 GPa on Z [2]. The results of these experiments challenge the controversial NOVA laser data [3,4] which show significantly increased compressibility compared to predictions of first principles, ab initio EOS models for the hydrogen isotopes [5]. These Z measurements use the technique of magnetically driven planar flyer plate impact on relatively large area, thick samples, with multiple redundant diagnostics to improve accuracy and address many of the concerns over the experimental conditions of the laser measurements. 1141 Blast shield Figure 1 shows the arrangement of the LHe cryostat used to simultaneously cool two separate LD2 samples on the Z experiments. Survivability of high value cryogenic components is a major issue for cryogenic system design on Z. Following the current pulse, more than 1 MJ of energy is dissipated in the form of hot plasma, molten metal, and shrapnel ejected from the load region. The LHe cryostat is shock-mounted inside a robust stainless steel blast shield. Cryostats in this arrangement have survived many Z shots without significant damage. The design of the cryocell for LD2 shock Hugoniot measurements is shown in Fig. 2. The LD2 sample is condensed from high purity D2 gas at 18 psi in a cavity formed by a stepped Al pusher plate and a sapphire rear window. This window provides optical access for fiber-optic-coupled VISAR, active shock breakout, and time-resolved visible light spectroscopy diagnostic probes. The cryocell is thermally isolated from the anode mounting panel by a thin Nylon thermal break. Each cryocell is cooled to about 19 K and then warmed to 22.5 K by a combination of heater energy and absorbed diagnostic laser light to produce a quiescent (bubble-free) LD2 sample with a boiling point of about 24.7 K. Spatially uniform, constant pressure shock loading of the Al pusher is produced by impact of the flyer plate accelerated by magnetic pressure from a ramped current drive. LN2 reservoir Thermal insulator LHe level sensor LHe reservoir LHe reservoir tail 80 K shield Cold ingeiv , ISENTROPIC COMPRESSION OF LN2 We have recently demonstrated in studies of Cu and Fe that magnetic pressure loading with the ramped current pulse of the Z accelerator can be used to accurately determine the off-Hugoniot isentropic response of materials at high pressures [1]. The experimental arrangement being developed to extend this technique to an LN2 sample is shown in Fig. 3. A quiescent large area LN2 sample is condensed from high purity N2 gas at about 78 K in a cryocell similar to that shown in Fig. 2. Cooling is provided by the cryostat shown in Fig. 1, with each reservoir now filled with LN2. In an isentropic compression experiment, the Al pusher plate at the front of the cryocell forms part of the current path of the short circuit load and is gently accelerated by the magnetic pressure from a ramped, shaped current pulse, quasi-isentropically compressing the LN2. Cold j ,rfinger /*-|^A D2 cryocell 1 \ D2 cryocell 2 ICE panels FIGURE 1. Static-fill LHe cryostat with double cold finger for simultaneous cooling of two LD2 cryocells. 1142 LHe EOS MEASUREMENTS 4 He is the most fundamental of the permanent gases. This isotope has the smallest closed-shell atom with an extremely weak intermolecular potential and exhibits unique quantum properties in the liquid state. It is a component of many systems of astrophysical, condensed matter, and ICF interest. Very little EOS data exist for 4He at high pressures because of the difficulty of condensing quiescent liquid 4He samples at less than 4 K in an environment suitable for shock physics measurements. We are currently developing a variation of the Z cryogenic target system to condense superfluid 4 He-II samples at 1.5 K for He EOS measurements. The cryostat for this system is shown in Fig. 4. To minimize the heat load and maintain a stable sample environment at 1.5 K, the 4He sample holder must be surrounded by a double thermal radiation shield consisting of an outer layer cooled by LN2 to 80 K and an inner shield cooled by LHe to 5 K. These shields are segmented into overlapping sections, some of which serve as part of the cryostat blast shield. This acts to mechanically decouple the He sample holder from the main LHe cryostat and allow the survival of the most expensive cryogenic system components in the Z blast environment. The design of the sample holder assembly for LHe shock Hugoniot measurements with magnetically driven flyer plates is shown in Fig. 5. The sample holder is operated as a continuously fed 4He evaporation refrigerator [6]. The sample holder consists of a small LHe bath, which controls the cooling of the sample holder body, and a cavity at the front in which high purity 4He gas is condensed into a quiescent LHe sample for the experiment. LHe from the main cryostat at 4.2 K and 760 Torr is drawn through a flow impedance and partially evaporated to cool the LHe bath at 3.6 Torr to 1.5 K. * window M .fter MO FIGURE 2. Cryocell in magnetically driven flyer plate configuration for LD2 Hugoniot measurements. Ctiff$Hl line I IfKHHlt 1m SUMMARY ciamp We have briefly described several of the cryogenic sample capabilities being developed to complement new precision EOS Hugoniot and offHugoniot measurement techniques on Z. FIGURE 3. Cryocell design for isentropic compression of a LN2 sample. 1143 Crywtit blast break FIGURE 5. Sample holder assembly for condensing a superfluid 4He-II sample at 1.5 K for LHe Hugoniot measurements. ACKNOWLEDGMENTS Sandia is a multiprogram laboratory operated by Sandia Corporation, a Lockheed Martin Company, for the United States Department of Energy under Contract DE-AC04-94AL85000. REFERENCES 3. 4. 5. 6. FIGURE 4. Cryostat and radiation shielding for cooling the LHe sample holder assembly. 1144 J. R. Asay, "Isentropic Compression Experiments on the Z Accelerator," in Shock Compression of Condensed Matter-1999, edited by M. D. Furnish et al, AIP Conference Proceedings 505, New York, 2000, pp. 261-266. M. D. Knudson, et al, "Equation of State Measurements of Liquid Deuterium Subject to Magnetically Driven Hypervelocity Plate Impact," submitted to Phys. Rev. Lett. L. DaSilva, etal, Phys. Rev. Lett. 78, 483 (1997). G. W. Collins, et al, Science 281, 1178 (1998). T. J. Lenosky, etal, Phys. Rev. B56, 5164 (1997). L, E, DeLong, et al, Rev. Sci. Instrum. 42, 147 (1971).
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