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 EXPERIMENT TO CAPTURE GASEOUS PRODUCTS FROM SHOCK-DECOMPOSED MATERIALS W. H. Holt, W. Mock, Jr., F. Santiago, and R. M. Gamache Naval Surface Warfare Center, Dahlgren Division, 17320 Dahlgren Rd., Dahlgren, VA 22448-5100 Abstract. Vacuum-tight steel containers have been designed and impact tested for the purpose of capturing gaseous products from the shock decomposition of porous polymer materials. This work extends earlier gas gun experiments in which initially-porous polytetrafluoroethylene (PTFE) powder specimens were shock compressed inside closed non-vacuum-tight steel containers and soft recovered. Although a powder decomposition residue was produced in the containers and analyzed in situ, there was no attempt to recover any gaseous decomposition products for analysis. A series of gas gun impact experiments has now been performed to develop a gas-tight specimen container that can survive impact shock loading. The container is evacuated prior to the experiment. The impact of a gas-gunaccelerated metal disk produces a shock wave that passes through the container wall and into the specimen material. If gaseous products are formed, they can be collected in a sample cylinder for subsequent chemical analyses. Initial results are presented for PTFE powder specimens. carbon. Gas recovery experiments have also been performed on serpentine rock (4). The purpose of the current experiments is to extend our earlier work to the include capture of the gaseous products. INTRODUCTION Improved understanding of the response of materials to mechanical shock loading, and in particular, the shock-induced decomposition of materials, can lead to extensions of existing models for more realistic simulations of material response to a wide range of shock loading conditions. In our earlier experiments, initially-porous (4447% porosity) polytetrafluoroethylene (PTFE) powder specimens were shock compressed at initial planar stresses of 1.5 and 0.72 GPa, respectively, inside closed but unsealed steel containers, and soft recovered (1,2). X-ray photoelectron spectroscopy analysis of the solid residue indicated significant unbound carbon and a variety of other chemical species. No attempt was made to capture gaseous products, although visual evidence of the expulsion of solid products from the containers suggested the presence of gaseous products. Morris, et al, (3) in experiments at ~50 GPa, have reported evidence of shock-induced dissociation of initially-solid PTFE, leading to CF4 gas and a residue of amorphous EXPERIMENTAL TECHNIQUE Figure l(a) is a schematic of the experiment before impact. Figure l(b) shows the experiment at the time of impact. The Naval Surface Warfare Center Dahlgren Division Research Gas Gun Facility (5) was used for this work. The specimen container is attached to a steel support block, located 0.8 m from the muzzle of the 40.0 mm smoothbore barrel. The impactor disk is carried on the end of a sabot. A thin mica cover on the muzzle permits evacuation of the barrel prior to firing the gun. The sabot and impactor disk pass through the mica cover and through a hole in the support block to impact the specimen container. A steel cover disk and momentum trap disks were used to reduce damage to the container. 1196 The PTFE specimen material (6) was characterized with respect to initial particle morphology via optical and scanning electron microscopy, and was in the form of nearly spherical white particles having obvious surface substructures. The average particle size was 534 microns (7). In all the experiments, each specimen was pressed to have an initial porosity in the 44-47% range. VALVi RESULTS A series of experiments was performed with different specimen container designs to assess container survivability prior to attempting to capture product gases. The first container was a pair of 11.5-mm-thick stainless steel vacuum flanges (8) bolted together with a copper gasket seal and having a porous PTFE specimen disk (approximately 37mm diameter and 2.3mm thick) sandwiched between the flanges. A 4.6-mm-thick 6061-T6 aluminum disk impacted this container directly (no cover disk was used). Figure 2 shows one-half of the container before and after shock loading, with visual evidence of shock-induced chemical reaction (a) VALVE CLOSED VAtVi (a) (b) (b) FIGURE 2. Specimen disk in one-half of container, (a) Before impact, (b) After impact. The dark regions indicate shockinduced chemical changes. Impact speed was 986 m/s. FIGURE 1. (a) Schematic of gas collection experiment before impact. The impactor disk is accelerated on a sabot in a gas gun. Impact of the disk produces a shock wave that passes through the cover disk and container wall and into the specimen material. The cover disk receives the primary damage of impact. The system is evacuated prior to impact, and the sample cylinder is maintained at liquid nitrogen temperature to minimize any subsequent reactions of collected gaseous products. All the tubing, fittings, and valves are made of 316 stainless steel, (b) Schematic of gas collection experiment at time of impact. The valve connected to the sample cylinder is closed after impact so that the captured gas sample can be removed for analysis. in the specimen (dark regions). Because of damage to the bolts and to the copper gasket, this configuration did not retain a gas-tight seal. Figure 3 shows parts for an experiment with an alternate specimen container design. To fabricate the container, a 4.6-mm-diameter hole was drilled radially into the center of a 76.1-mm-diameter, 1197 the flat end of the 31.9-mm-thick solid cylinder. The tube is deformed inside the solid cylinder, compressing the specimen material. Figure 4 shows this container design mounted near the gas gun muzzle for impact. The gas collection system (Figure 1) was attached to this configuration in an attempt to capture gaseous products. The pressed porous specimen filled a 28.6-mm-thick solid cylinder of 4130 steel. A stainless steel tube fitting was welded into the hole to provide a gas connection. PTFE powder was pressed into the hole. For this experiment a 3.1mm-thick, 35.6-mm-diameter OFHC copper disk impacted the 9.53-mm-thick steel cover disk at 976 m/s. This container survived impact and appeared to be free of cracks affecting the specimen cavity. A residue of partially-reacted PTFE was found in the cavity. Another container design consisted of a 316 stainless steel tube (9.7 mm outside diameter, 7.5 mm inside diameter) that fits through a centered diametric hole in a solid cylinder of 4130 steel. A 9.5-mm-thick steel cover disk was placed against FIGURE 4. Cylinder and tube container mounted on the support system for connection to the gas collection system and impact. All the tubing and fittings were made of 316 stainless steel. 25-mm-long region of the gas collection tube and was centered with respect to the axis of the gas gun barrel. Connection was made to both ends of the straight tube to facilitate evacuation of the specimen region. The container was evacuated by a turbomolecular pumping system to 1.5 x 10"6 Torr, measured by an ion gauge near the pump. The gas collection system was baked at ~125°C, while the specimen container was kept at -25°C to minimize thermally-induced changes in the specimen. A 3.1mm-thick OFHC copper disk impacted the configuration at 977 m/s. As shown in Figure 1, product gases were collected in a sample cylinder (9) that was immersed in liquid nitrogen. Figure 5 shows the container after impact. The impact side was deformed but had no visible fractures. The post-impact pressure in the system was in the 10~4 Torr range. The tube contained a residue that was partially-reacted PTFE. Preliminary mass spectrometric analyses of the captured gas from this experiment have been (c) FIGURE 3. (a) Parts for experiment before impact, (b) Deformed container after impact. This container had one visible crack near the edge that did not affect the specimen cavity, (c) Deformed and fractured cover disk for container. Impact speed was 976 m/s. 1198 were performed using a residual gas analyzer. One of the observed strong spectral lines corresponded to the mass of a gaseous fluorine compound, trifluoromethane (CHF3). performed using a residual gas analyzer (RGA). A background spectrum was first obtained for the RGA at 10~6 Torr. When small samples of the captured gas were leaked into the RGA, the ACKNOWLEDGEMENT This work was supported by the In-House Laboratory Independent Research Office of the Naval Surface Warfare Center, Dahlgren Division. REFERENCES 1. Mock, W. Jr., Holt, W. H., and Kerley, G. I., "Shock and Recovery of PTFE Powder," in Shock Compression of Condensed Matter-1997, edited by S. C. Schmidt et al, AIP Conference Proceedings 429, New York, 1998, pp. 671-674. 2. Holt, W. H., Mock, W. Jr., and Santiago, F., J. Appl Phys. 88, 5485-5486 (2000). 3. Morris, C. E., Fritz, J. N., and McQueen, R. G., J. Chem. Phys. 80, 5203-5217 (1984). 4. Tyburczy, J. A., Krishnamurthy, Epstein, S. and Ahrens, T. J., Earth Planet. Sci. Lett. 98, 245-260 (1990). 5. W. Mock, Jr. and W. H. Holt, The NSWC Gas Gun Facility for Shock Effects in Materials, NSWC/DL TR3473, Naval Surface Weapons Center, Dahlgren, VA 22448, July 1976. 6. The material was DuPont Type 8B Teflon PTFE powder, purchased from E. I. du Pont de Nemours and Company, Wilmington, DE 19898. Teflon is a registered trademark of DuPont. 7. Average particle size information provided by Dupont Certification Office, P.O. Box 1217, Parkersburg, WV 26102-1217. 8. Varian Conflat® Flange, 316 stainless steel, Part No. F02750000NC6. Varian Vacuum Technologies, 121 Hartwell Avenue, Lexington, MA 02421-3133. 9. Whitey Miniature Sample Cylinder, Single Ended, No. SS-4CS-TW-25. Whitey Co., Highland Heights, OH 44143.1490. 10. The Condensed Chemical Dictionary, 9th Ed., edited by G. G. Hawley, Van Nostrand Reinhold Company, New York, 1977, p.391. FIGURE 5. Cylinder and tube container after impact. The tube was deformed but not fractured and remained vacuum-tight. Impact speed was 977 m/s. spectra showed a variety of additional peaks, mostly corresponding to higher masses than were observed in the background spectrum. These measurements were repeated eight times with consistent results. One of the strong peaks in each of the sample spectra corresponded to the mass for trifluoromethane (CHF3), which has a boiling point of-84°C (1 atm) (10). These results are considered preliminary since the post-impact solid residue appeared to be only partially reacted. Additional experiments are planned to include higher impact stresses and longer stress durations, along with analyses using a higher resolution mass spectrometer. SUMMARY A series of impact experiments has been performed using different specimen container designs to develop a configuration that would permit capture of product gases from shock-decomposed materials. For one of the experiments a gas collection system was connected to the specimen container. Gaseous products were collected in an evacuated sample cylinder. Preliminary mass spectrometric analyses 1199
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