Zeitschriftenartikel: „Light gas gun“

1

Tidman, D. A., und D. W. Massey. „Electrothermal light gas gun“. IEEE Transactions on Magnetics 29, Nr. 1 (Januar 1993): 621–24. http://dx.doi.org/10.1109/20.195647.

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2

Wang, Bai Qiu, Cong Wang, Hai Long Huang, Yan Jiang Xing und Jia Zhong Zhang. „Analysis of Underwater Projectile Experiment Using One Stage Light Gas Gun and Numerical Simulation“. Applied Mechanics and Materials 226-228 (November 2012): 776–79. http://dx.doi.org/10.4028/www.scientific.net/amm.226-228.776.

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One stage light gas gun is an important device for experiments of low-speed supercavitation projectiles. After a reasonable simplification to the gas gun, movements of the projectile in the barrel have been analyzed and the relationships between the initial pressure of the gas gun and the exit velocity of the projectile were obtained. For meeting the velocity difference between at the gun exit and water-entry, a speed impairment factor was employed. The results of the adiabatic analysis of the simplified gun show that the best ratio between gun chamber volume and the barrel length is related to the gas thermodynamic process and the gas residual pressure has relation to the gas thermodynamic process. The low-speed supercavitation projectile experiments have been carried out. The movements of the projectile in the gas gun and the supercavitation shape and projectile speed after water-entry have been numerically simulated.

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3

Linhart, J. G., und F. Cattani. „Theory of a multistage light gas gun“. Acta Astronautica 61, Nr. 7-8 (Oktober 2007): 617–25. http://dx.doi.org/10.1016/j.actaastro.2006.12.008.

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4

Liu, Yang, Xiao Dong Song, Xiao Xian Yao und Kun Li. „Dynamic Simulation and Experimental Research of High Pressure Pneumatic Valve in Gas-Driven Light Gas Gun“. Applied Mechanics and Materials 365-366 (August 2013): 289–93. http://dx.doi.org/10.4028/www.scientific.net/amm.365-366.289.

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Use gas-driven light gas gun is one of the techniques extensively used to achieve hypervelocity projectiles. The device was made up of a compressed gas gun as the first-stage drive. A new type high pressure pneumatic injecting system of gas-driven light gas gun for hypervelocity launching is introduced. As a critical component of the injecting system, the high pressure pneumatic valve was designed. Functions of the pneumatic valve were preserved and relevant techniques were discussed. Besides, a high pressure pneumatic mass flow control test-bed using inert medium was built in order to study the dynamic response characteristic of high pressure pneumatic valve in gas-driven light gas gun. To ascertain the response delay time of the valve, several turn-on and turn-off experimental tests of the valve were initiated. The results suggest that: the pressure of pneumatic electromagnetic valve gas supply circuit seriously influenced the properties of high pressure pneumatic valve; the mean delay time of the high pressure pneumatic valve was 190ms approximately at 6.5MPa gas pressure of the pneumatic electromagnetic valve gas supply circuit.

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5

AKAHOSHI, Yasuhiro, Yousuke SATO und Takushi KAJITANI. „Effectiveness of Mixed Gas in Two-Stage Light Gas Gun“. Proceedings of Conference of Kyushu Branch 2002.55 (2002): 41–42. http://dx.doi.org/10.1299/jsmekyushu.2002.55.41.

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6

Lamberson, L. E., und P. A. Boettcher. „Compressed gas combined single- and two-stage light-gas gun“. Review of Scientific Instruments 89, Nr. 2 (Februar 2018): 023903. http://dx.doi.org/10.1063/1.5000912.

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7

TSUTSUMI, Toshiaki, Katsuhiro OKUMURA, Nobuyoshi MATSUSHITA und Yasuhiro AKAHOSHI. „208 Improvement of Two-Stage Light Gas Gun“. Proceedings of Conference of Kyushu Branch 2000.53 (2000): 31–32. http://dx.doi.org/10.1299/jsmekyushu.2000.53.31.

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8

Laabs, Gary W., David J. Funk und Blaine W. Asay. „Novel light gas gun with minimal timing jitter“. Review of Scientific Instruments 67, Nr. 1 (Januar 1996): 195–97. http://dx.doi.org/10.1063/1.1146570.

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9

Sorrell, F. Y., und M. D. Smith. „Dynamic structural loading using a light gas gun“. Experimental Mechanics 31, Nr. 2 (Juni 1991): 157–62. http://dx.doi.org/10.1007/bf02327569.

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10

OKUMURA, Katsuhiro, Yasuhiro AKAHOSHI, Toshiaki TSUTSUMI und Nobuyoshi MATSUSHITA. „209 Development of Desktop Two-Stage Light Gas Gun“. Proceedings of Conference of Kyushu Branch 2000.53 (2000): 33–34. http://dx.doi.org/10.1299/jsmekyushu.2000.53.33.

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11

AKAHOSHI, Yasuhiro, Katsuhiro OKUMURA und Yousuke SATO. „207 Development of Desktop Two-Stage Light Gas Gun“. Proceedings of Conference of Kyushu Branch 2001.54 (2001): 47–48. http://dx.doi.org/10.1299/jsmekyushu.2001.54.47.

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12

Moritoh, Tatsumi, Nobuaki Kawai, Kazutaka G. Nakamura und Ken-ichi Kondo. „Three-stage light-gas gun with a preheating stage“. Review of Scientific Instruments 75, Nr. 2 (Februar 2004): 537–40. http://dx.doi.org/10.1063/1.1641155.

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13

Fellows, N. A., und P. C. Barton. „Royal Military College of Science light gas gun facility“. Review of Scientific Instruments 68, Nr. 10 (Oktober 1997): 3823–27. http://dx.doi.org/10.1063/1.1148034.

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14

Rahner, C., H. A. Al-Qureshi, D. Stainer, D. Hotza und M. C. Fredel. „Numerical Evaluation of a Light-Gas Gun Facility for Impact Test“. Modelling and Simulation in Engineering 2014 (2014): 1–6. http://dx.doi.org/10.1155/2014/501434.

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Experimental tests which match the application conditions might be used to properly evaluate materials for specific applications. High velocity impacts can be simulated using light-gas gun facilities, which come in different types and complexities. In this work different setups for a one-stage light-gas gun facility have been numerically analyzed in order to evaluate their suitability for testing materials and composites used as armor protection. A maximal barrel length of 6 m and a maximal reservoir pressure of a standard industrial gas bottle (20 MPa) were chosen as limitations. The numerical predictions show that it is not possible to accelerate the projectile directly to the desired velocity with nitrogen, helium, or hydrogen as propellant gas. When using a sabot corresponding to a higher bore diameter, the necessary velocity is achievable with helium and hydrogen gases.

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15

Tang, Weiqi, Qiu Wang, Bingchen Wei, Jiwei Li, Jinping Li, Jiahao Shang, Kun Zhang und Wei Zhao. „Performance and Modeling of a Two-Stage Light Gas Gun Driven by Gaseous Detonation“. Applied Sciences 10, Nr. 12 (25.06.2020): 4383. http://dx.doi.org/10.3390/app10124383.

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A two-stage light gas gun driven by gaseous detonation was newly constructed, which can make up for the disadvantages of the insufficient driving capability of high-pressure gas and the constraints of gunpowder. The performance of the gas gun was investigated through experiments and a quasi-one-dimensional modeling of it was also developed and described in detail. The model accounts for the friction and heat transfer to the tube wall for gases by adding a source term. An improved model has been established to consider the inertial loads in the piston or projectile and model the friction force with the tube wall. Besides, the effects of pump tube pressure on the performance of the gas gun are also investigated numerically. Simulations of the pressure histories in the pump tube and the piston and projectile velocities were conducted. A good agreement was observed between the computational predictions and experimental results. The results showed that the friction between the piston and wall had only small influence on the piston velocity. The proposed numerical approach is suitable for the development of two-stage light gas guns and tests of the operating conditions.

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16

Schonberg, William P., und David Cooper. „Repeatability and uncertainty analyses of light gas gun test data“. AIAA Journal 32, Nr. 5 (Mai 1994): 1058–65. http://dx.doi.org/10.2514/3.12094.

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17

Huneault, Justin, Jason Loiseau, Myles Hildebrand und Andrew Higgins. „Down-Bore Velocimetry of an Explosively Driven Light-Gas Gun“. Procedia Engineering 103 (2015): 230–36. http://dx.doi.org/10.1016/j.proeng.2015.04.031.

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18

M., Aziz, Yakout H. und Riad M. „INTERNAL BALLISTIC SOLUTION OF A TWO-STAGE LIGHT-GAS GUN“. International Conference on Aerospace Sciences and Aviation Technology 12, ASAT CONFERENCE (01.05.2007): 1–13. http://dx.doi.org/10.21608/asat.2007.23877.

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19

Hawke, R. S., A. R. Susoeff, J. R. Asay, J. A. Ang, C. A. Hall, C. H. Konrad, G. W. Wellman et al. „Railgun performance with a two-stage light-gas gun injector“. IEEE Transactions on Magnetics 27, Nr. 1 (Januar 1991): 28–32. http://dx.doi.org/10.1109/20.100988.

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20

Pavarin, Daniele, und Alessandro Francesconi. „Improvement of the CISAS high-shot-frequency light-gas gun“. International Journal of Impact Engineering 29, Nr. 1-10 (Dezember 2003): 549–62. http://dx.doi.org/10.1016/j.ijimpeng.2003.10.004.

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21

Putzar, Robin, und Frank Schaefer. „Concept for a new light-gas gun type hypervelocity accelerator“. International Journal of Impact Engineering 88 (Februar 2016): 118–24. http://dx.doi.org/10.1016/j.ijimpeng.2015.09.009.

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22

Tadaoka, M., Y. Akahoshi, T. Koura, S. Fukusige, E. Matude, J. Kitagawa und Y. Qu. „Preliminary study of counter impact with two-stage light gas gun using electrothermal–chemical gun technology“. International Journal of Impact Engineering 33, Nr. 1-12 (Dezember 2006): 11–23. http://dx.doi.org/10.1016/j.ijimpeng.2006.09.013.

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23

TANNO, Hideyuki, Tomoyuki KOMURO, Masatoshi KODERA, Kazuo SATO und Katsuhiro ITOH. „Free-Flight Testing in the Gas-Driven Two-Stage Light Gas Gun HEK-G“. TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN 10, ists28 (2012): Tr_41—Tr_45. http://dx.doi.org/10.2322/tastj.10.tr_41.

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24

Zhang Ningchao, 张宁超, 任娟 Ren Juan, 王鹏 Wang Peng und 刘福生 Liu Fusheng. „Radiation Spectral Characteristics of Sapphire Under Light-Gas Gun Impact Loading“. Acta Optica Sinica 38, Nr. 5 (2018): 0530002. http://dx.doi.org/10.3788/aos201838.0530002.

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25

Bogdanoff, David W. „Optimization study of the Ames 0.5″ two-stage light gas gun“. International Journal of Impact Engineering 20, Nr. 1-5 (Januar 1997): 131–42. http://dx.doi.org/10.1016/s0734-743x(97)87487-8.

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26

Angrilli, F., D. Pavarin, M. De Cecco und A. Francesconi. „Impact facility based upon high frequency two-stage light-gas gun“. Acta Astronautica 53, Nr. 3 (August 2003): 185–89. http://dx.doi.org/10.1016/s0094-5765(02)00207-2.

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27

Combs, S. K., C. R. Foust, D. T. Fehling, M. J. Gouge und S. L. Milora. „Repetitive two‐stage light gas gun for high‐speed pellet injection“. Review of Scientific Instruments 62, Nr. 8 (August 1991): 1978–89. http://dx.doi.org/10.1063/1.1142402.

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28

FUKUSHIGE, Shinya, Yasuhiro AKAHOSHI, Naomi FURUSAWA, Takao KOURA und Shoji HARADA. „1027 Muzzle velocity improvement of small two-stage light gas gun“. Proceedings of the JSME annual meeting 2006.5 (2006): 347–48. http://dx.doi.org/10.1299/jsmemecjo.2006.5.0_347.

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29

Vinyar, I. V., und A. N. Shlyakhtenko. „Ablation of a hydrogen pellet in a light-gas gun bore“. Fluid Dynamics 34, Nr. 1 (Januar 1999): 1–8. http://dx.doi.org/10.1007/bf02698743.

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30

Grosch, Donald J., und Jack P. Riegel. „Development and optimization of a “micro” two-stage light-gas gun“. International Journal of Impact Engineering 14, Nr. 1-4 (Januar 1993): 315–24. http://dx.doi.org/10.1016/0734-743x(93)90030-b.

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31

Sekine, T., und T. Kobayashi. „NIRIM two-stage light–gas gun and equation of state of carbides“. Journal of Materials Processing Technology 85, Nr. 1-3 (Januar 1999): 11–14. http://dx.doi.org/10.1016/s0924-0136(98)00245-3.

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32

Putzar, Robin, und Frank Schaefer. „EMI's TwinGun Concept for a New Light-gas Gun Type Hypervelocity Accelerator“. Procedia Engineering 103 (2015): 421–26. http://dx.doi.org/10.1016/j.proeng.2015.04.041.

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33

KATO, Hiroaki, Masahiro NISHIDA, Koichi HAYASHI und Kayoko KUZUYA. „754 Shortening of Sabot Separation Distance of Two-Stage Light Gas Gun“. Proceedings of Conference of Tokai Branch 2011.60 (2011): _754–1_—_754–2_. http://dx.doi.org/10.1299/jsmetokai.2011.60._754-1_.

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34

Martin, L. Peter, J. Reed Patterson, Daniel Orlikowski und Jeffrey H. Nguyen. „Application of tape-cast graded impedance impactors for light-gas gun experiments“. Journal of Applied Physics 102, Nr. 2 (15.07.2007): 023507. http://dx.doi.org/10.1063/1.2756058.

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35

Goodwin, P. M., B. D. Bartram, L. L. Gibson, M. Wu und D. M. Dattelbaum. „Non-invasive timing of gas gun projectiles with light detection and ranging“. Journal of Physics: Conference Series 500, Nr. 14 (07.05.2014): 142009. http://dx.doi.org/10.1088/1742-6596/500/14/142009.

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36

CHANG, Xinyu, Kouji SHIMOMURA und Shiro TAKI. „Development and Performance Examination of a Two-Stage Detonation Light Gas Gun.“ Transactions of the Japan Society of Mechanical Engineers Series B 62, Nr. 599 (1996): 2819–25. http://dx.doi.org/10.1299/kikaib.62.2819.

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37

Xu, Xin, Lin Wang, Deng Hui Zhao und Wen Wen Du. „Dynamic Behavior in Ti-5553 Alloy with β Phase under Compression Loading“. Applied Mechanics and Materials 782 (August 2015): 88–96. http://dx.doi.org/10.4028/www.scientific.net/amm.782.88.

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In this paper, the shock phase transformation of β phase in Ti-5Al-5Mo-5V-3Cr-0.5Fe (Ti-5553) was investigated. Split Hopkinson Pressure Bar (SHPB) and light gas gun were employed to investigate the dynamic properties under high strain rates from 1000s-1to 3500s-1. Microstructure characterization was carried out by optical microscopy (OM), scanning electronic microscopy (SEM) and transmission electron microscope (TEM). The experimental results demonstrate that the Ti-5553 alloy with β phase exhibit no obvious strain rate hardening effect with the high strain rate from 1000s-1to 3000s-1. However, compared with the quasi-static compression test results (10-3s-1), this alloy shows an evident strain rate hardening effect, with the yield strength significantly improved. Second time loading indicates light gas gun dynamic tensile loading and then SHPB dynamic compression loading in Ti-5553 alloy with β phase. The results show that the shock-induced β to αʺ martensite phase transformation dramatically influences the postshock mechanical properties of these alloys. The yield strength of this alloy decreased after the shock wave effect of light gas gun, its ductility increasing. Higher shock pressures yielded an increased dislocation density and a gradual increase in the yield strength. Adiabatic shear band (ASB) exists in second time loading Ti-5553 alloy under 103s-1strain rate. SHPB loaded the alloy: The results show that the Ti5553 alloy with β phase is adiabatic shear failure in high strain rate (3000s-1).

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38

Mieno, Tetsu, Kazuki Ookouchi, Kazuhiko Kondo, Susumu Hasegawa und Koichi Kurosawa. „Production of Carbonaceous Molecules by the Impact Reaction in Nitrogen Gas by Use of a Gas-Gun“. Advanced Materials Research 1117 (Juli 2015): 31–34. http://dx.doi.org/10.4028/www.scientific.net/amr.1117.31.

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In order to investigate impact production of carbonaceous molecules by asteroid’s impact, simulation experiment is carried out using a 2-stage light gas-gun. A small polycarbonate bullet is injected into a pressurized chamber with 1 atm of nitrogen gas, to collide with a target. Strong emissions of CN and C2 molecules are measured, and CN rotational temperature is evaluated. In the produced soot, production of fullerenes, nanotubes, metal-encapsulated particles, balloon-like nano-carbons and amino acids is confirmed.

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39

Yin, Jun, Yu Wang Yang, Xia Yun Hu und Cheng Cheng Yong. „A Hypervelocity Impact Facilities Based on Double-Barreled Two-Stage Light Gas Gun“. Advanced Materials Research 834-836 (Oktober 2013): 825–28. http://dx.doi.org/10.4028/www.scientific.net/amr.834-836.825.

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For almost all materials the hypervelocity regime has been reached when the impact speed above 2 km/s. A double-barreled two-stage light gas gun (TSLGG) system used for the hypervelocity impact tests is described. The proposed TSLGG can accelerate 50 g projectile masses up to velocities of 2.2 km/s. The craters produced with this equipment reach a diameter of up to 20 cm, a size unique in laboratory cratering research. The experiment results show our TSLGG system work effectively, velocity of the projectile mass is measured highly accurate by means of the proposed optical method.

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40

MATSUMURA, Tomoharu, Kazuyoshi TAKAYAMA und James J. GOTTLIEB. „A numerical study of the performance of a two-stage light gas gun.“ Transactions of the Japan Society of Mechanical Engineers Series B 56, Nr. 526 (1990): 1712–15. http://dx.doi.org/10.1299/kikaib.56.1712.

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41

de Icaza, M., C. Renero und F. E. Prieto. „Design operation and test of a light gas gun in a developing country“. Review of Scientific Instruments 60, Nr. 10 (Oktober 1989): 3284–92. http://dx.doi.org/10.1063/1.1140567.

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42

Hawke, R. S., J. R. Asay, C. A. Hall, R. J. Hickman, C. H. Konrad, J. L. Sauve und A. R. Susoeff. „Armature formation in a railgun using a two-stage light-gas gun injector“. IEEE Transactions on Plasma Science 17, Nr. 3 (Juni 1989): 378–85. http://dx.doi.org/10.1109/27.32245.

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43

Gerasimov, S. I., V. I. Erofeev, V. G. Kamchatyi und V. A. Kikeev. „Transverse Motion of a Projectile in the Barrel of a Light-Gas Gun“. Russian Engineering Research 38, Nr. 2 (Februar 2018): 80–85. http://dx.doi.org/10.3103/s1068798x18020089.

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44

MIENO, Tetsu, und Sunao HASEGAWA. „Titan Satellite Would Be a Carbon-Cluster Factory -From Light-Gas Gun Experiment-“. TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, SPACE TECHNOLOGY JAPAN 7, ists26 (2009): Tr_2_75—Tr_2_78. http://dx.doi.org/10.2322/tstj.7.tr_2_75.

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45

SHIROUZU, Masao, Kunio SOGA und Takashi YAMAZAKI. „An application of Random-Choice-Method to Two-Stage Light-Gas Gun simulation.“ Journal of the Japan Society for Aeronautical and Space Sciences 34, Nr. 389 (1986): 325–31. http://dx.doi.org/10.2322/jjsass1969.34.325.

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46

Combs, S. K., C. R. Foust, M. J. Gouge und S. L. Milora. „Acceleration of small, light projectiles (including hydrogen isotopes) to high speeds using a two‐stage light gas gun“. Journal of Vacuum Science & Technology A: Vacuum, Surfaces, and Films 8, Nr. 3 (Mai 1990): 1814–19. http://dx.doi.org/10.1116/1.576808.

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47

Zheng, Jian-Dong, Jin-Chao Niu, Hong-Xian Zhong, Zi-Zheng Gong und Yan Cao. „Hypervelocity impact damage properties of solar arrays by using two-stage light gas gun“. Acta Physica Sinica 68, Nr. 22 (2019): 220201. http://dx.doi.org/10.7498/aps.68.20191132.

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48

Lamberson, Leslie. „Investigations of High Performance Fiberglass Impact Using a Combustionless Two-stage Light-gas Gun“. Procedia Engineering 103 (2015): 341–48. http://dx.doi.org/10.1016/j.proeng.2015.04.056.

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49

Shahinpoor, M., J. R. Asay, C. H. Konrad und C. A. Hall. „Use of a two-stage light-gas gun as an injector for electromagnetic railguns“. IEEE Transactions on Magnetics 25, Nr. 1 (1989): 514–18. http://dx.doi.org/10.1109/20.22592.

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50

Yep, Steven J., Jonathan L. Belof, Daniel A. Orlikowski und Jeffrey H. Nguyen. „Fabrication and application of high impedance graded density impactors in light gas gun experiments“. Review of Scientific Instruments 84, Nr. 10 (Oktober 2013): 103909. http://dx.doi.org/10.1063/1.4826565.

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Zeitschriftenartikel zum Thema „Light gas gun“

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