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Title:
THE HIGH-POWER ARC-JET PLASMA GENERATOR (PLASMA TORCH) CHARACTERISTICS AND PERFORMANCE

Authors:
Sedanur Toraman, T. Yasar Katircioglu, Caglar Terzi

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2PhD., Chemistry, ARTECS Anadolu R&D Technology Engineering and Consultancy Inc.
3PhD. Candidate, Computer Engineering, ARTECS Anadolu R&D Technology Engineering and Consultancy Inc.

MLA 8
Toraman, Sedanur, et al. "THE HIGH-POWER ARC-JET PLASMA GENERATOR (PLASMA TORCH) CHARACTERISTICS AND PERFORMANCE." IJETSI, vol. 2, no. 4, 2017, pp. 680-699, ijetsi.org/more2017.php?id=56.
APA
Toraman, S., Kat?rc?oglu, T. Y., & Terzi, C. (2017). THE HIGH-POWER ARC-JET PLASMA GENERATOR (PLASMA TORCH) CHARACTERISTICS AND PERFORMANCE. IJETSI, 2(4), 680-699. Retrieved from http://ijetsi.org/more2017.php?id=56
Chicago
Toraman, Sedanur, T. Y. Katircioglu, and Caglar Terzi. "THE HIGH-POWER ARC-JET PLASMA GENERATOR (PLASMA TORCH) CHARACTERISTICS AND PERFORMANCE." IJETSI 2, no. 4 (2017), 680-699. http://ijetsi.org/more2017.php?id=56.

References
References
[1] Bottin, B., Chazot, O., Carbonaro, V., Van Der Heagen, V., Paris, S. The VKI plasmatron characteristics and performance. North Atlantic Treaty Organization. 1999.
[2] Pessin, M., Butler, J., Sparks, J. S. (2009) Thermal Protection System. Retrieved February, 2017 from https://www.nasa.gov/centers/johnson/pdf/5 84728main_Wings- ch4b- pgs182-199.pdf
[3] Svirchuk, Y. S., Golikov, A. N. Threephase Zvezda- type plasmatrons. IEEE Transactions on Plasma Science, Vol. 44, No. 12, 2016. 3042-3047.
[4] Katircioglu, T. Y., (2014). Komur Gazlastirma. Plazma Teknolojileri (155- 167) Ankara, irun Yayinlari
[5] Karpenko, E. I., Karpenko, Yu. E., Messerle, V. E., Ustimenko, A. B. (2009). Use of plasma fuel systems at thermal plants in Russia, Kazakhstan, China, and Turkey. High Energy Chemistry, Vol.43, No. 3, 224- 228
[6] Fabry, F., Rehmet, C., Rohani, V., Fulcheri, L. Waste gasification by thermal plasma: a review, waste and biomass valorization, (2013). 4 (3), 421-439.
[7] Zhukov, M. F., and Zasypkin, I. M. Thermal plasma torches design, characteristics, applications. Cambridge International Science Publishing. (2007). 399-410.
[8] Yamada, T., and Inatani, Y. Arc heating facility and for planetary entry test technique missions, The Institute of Space and Astronautical Science Report SP (2003). No. 17.147-163.
[9] Koroteev, A. S., Mironov, V. M., and Svirchuk, Y. S.Plasmatrons-design, characteristics, calculations, (in Russian). Moscow:Mashinostroenie, (1993). 296.
[10] Rutberg, Ph G., Safronov, A. A., Popov, S. D., Surov, A. V., Nakonechny, Gh. V. Multiphase stationary plasma generators working on oxidizing media. Plasma Phys. Control. Fusion 47 (2005) 1681- 1696.
[11] Ozge Yazicioglu, T. Yasar Katircioglu, Beycan Ibrahimoglu, "Optik Emisyon Spektrometre Kullanarak Yuksek Guclu Bir Plazmatron Plazma Akisi Sicaklik Olcumu", Surdurulebilir Havacilik Arastirmalari Dergisi, SUHAD, Cilt 2, Sayi 1, 2017
[12] Xiao-Zhi, S., Ping, Y., Hua-Ming, Z., and Jie, W. Transition probabilities for NII 2p4f-2p3d and 2s2p23d-2s2p23p obtained by a semiclassical Method. Chinese Physics, (2007). Vol 16 No 10, 16(10)/2934-04
[13] National Institute of Standards and Technology. Retrieved February, 2017 from https://www.nist.gov/pml/atomic- spectradatabase
[14] Chazot, O., Panerai, F., Muylaert, J. Catalysis phenomena determination in plasmatron facility for flight experiment design. 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. (2010).
[15] Hall, N., (2015). Schlieren system. Retrieved February, 2017 fromhttps://www.grc.nasa.gov/WWW/K- 12/airplane/tunvschlrn.html
[16] Chazot, O., Gomes, J. M. P., Carbonaro, M. Characterization of a "Miniplasmatron" facility by pitot probe measurements. American Institute of Aeronautics and Astronautics, Inc.
[17] Ristic, S., Isakovic, J., Ilic, B., Ocokoljic, G. (2004). Review of methods for flow velocity measurement in wind tunnels. Scientific-Technical Review, (1998). Vol. LIV, No. 3, 60-71.
[18] Hare, A. L. Velocity measurement in plasma flows using cooled pitot tubes: an unsolved problem. (1977). Proceedings of the 3rd International Symposium on Plasma Chemistry,G3.1, Limoges.
[19] Porterie, B., Larini, M., Loraud, J-C. Cooled pitot tube in plasma jet: an impactpressure recovery model. (1994). Journal of Thermophysics and Heat Transfer, Vol. 8, No. 3. 385-392.
[20] Lumens, J. F. Bottin, B., Carbonaro, M. Design of a steady-state heat flux probe for measurements in an induction-heated plasma flow [wind tunnels]. ICIASF'97 Record. International Congress on Instrumentation in Aerospace Simulation Facilities, 410-419.
[21] Chen, F. F. (2003). Langmuir probe diagnostics. Retrieved February, 2017 from http://www.seas.ucla.edu/~ffchen/Publs/Che n210R.pdf

Abstract:
Nowadays, because of the unique and interesting features of plasmas, there is an increasingly wide range of applications in plasma technology. Plasmatron is an electro-technology device that converts electrical energy into heat energy. Medicine, energy, metallurgy, textile, aerospace technologies, thermochemical processes such as gasification and combustion processes are given examples of usage area of plasmatrons. In these processes, the plasmatron becomes an energy producer for the system and the requirement of hydrocarbon based fuel for combustion systems is eliminated. This paper highlights the importance of the characteristics and performance of the high-power arc-jet plasma torch and the diagnostics of plasma such as probes and other measurement devices to be used. In this study, as the plasma characteristics inside the plasmatron which means plasma parameters in the mixing chamber, pressure was directly measured, chamber temperature was calculated by using Gas Dynamic Method. In addition to the determination of internal parameters of plasmatron, two main intrusive measurement techniques which are the Pitot probe and the calorimetric heat flux probe were used in order to measure and characterize the plasmatron flame. In this paper, the main structure of a high-power plasma torch with power over 1 MW is summarized and the test methodology and the results obtained during the tests are also presented. The average values obtained at a power level about 1000 kW from our tests are given as following: the plasmatron chamber temperature above 4000 K, the plasmatron chamber pressure above 14.00 bar, and heat flux above 6.50 Mcal/kg.m2 .

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