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NTIS 바로가기한국추진공학회지 = Journal of the Korean Society of Propulsion Engineers, v.25 no.3, 2021년, pp.89 - 100
강철웅 (School of Mechanical Engineering, Chungbuk National University) , 황동현 (School of Mechanical Engineering, Chungbuk National University) , 안종현 (School of Mechanical Engineering, Chungbuk National University) , 이준서 (School of Mechanical Engineering, Chungbuk National University) , 이다인 (School of Mechanical Engineering, Chungbuk National University) , 안규복 (School of Mechanical Engineering, Chungbuk National University)
This paper deals with the construction of a combustion test facility and preliminary tests for hot-firing tests of a methane engine. First, the combustion test facility for a 1 kN-class thrust chamber using liquid oxygen/gas methane as propellants was designed and built. Before hot-firing tests, the...
Morehead, R.L., "Project Morpheus Main Engine Development and Preliminary Flight Testing," 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, San Diego, C.A., U.S.A, AIAA 2011-5927, Jul. 2011.
Melcher, J.C. and Morehead, R.L., "Combustion Stability Characterisrics of the Project Morpheus Liquid Oxygen/Liquid Methane Main Engine," 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Cleveland, O.H., U.S.A, AIAA 2014-3681, Jul. 2014.
Melcher, J. and Allred, J., "Liquid Oxygen/Liquid Methane Test Results of the RS-18 Lunar Ascent Engine at Simulated Altitude Conditions at NASA White Sands Test Facility," 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Denver, C.O., U.S.A, AIAA 2009-4949, Jun. 2012.
Rudnykh, M., Carapellese, S., Liuzzi, D., Arione, L., Caggiano, G., Bellomi, P., D'Aversa, E., Pellegrini, R., Lobov, S.D., Gurtovoy, A.A. and Rachuk, V.S., "Development of LM10-MIRA LOX/LNG expander cycle demonstrator engine," Acta Astronautica, Vol. 126, pp. 364-374, 2016.
Iannetti, A., Girard, N., Tchou-kien, D., Bonhomme, C., Ravier, N. and Edeline, E., "Prometheus, a LOX/LCH 4 Reusable Rocket Engine," 7th European Conference for Aeronautics and Space Sciences, Milano, Italy, EUCASS 2017-537, Jul. 2017.
Simontacchi, P., Blasi, R., Edeline, E., Sagnier, S., Ravier, N., Espinosa-Ramos, A., Breteau, J. and Altenhoefer, Ph., "Prometheus: Precursor of new low-cost rocket engine family," 8th European Conference for Aeronautics and Space Sciences, Madrid, Spain, EUCASS 2019-743, Jul. 2019.
Asakawa, H., Nanri, H., Aoki, K., Kubota, I., Mori, H., Ishikawa, Y., Kimoto, K., Ishihara, S. and Ishizaki, S., Chemical Rocket Propulsion: A Comprehensive Survey of Energetic Materials, Springer, Berlin, Germany, pp. 463-487, 2017.
Cho, Y.H. and Chang, H.S, "Hot Firing Tests of Liquid Rocket Engine Using LOX/LNG," 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Fort Lauderdale, F.L., U.S.A., Jul. 2004.
Kim, K.H. and Ju, D.S., "Development of 'chase-10' Liquid Rocket Engine having 10tf thrust using lox & lng (methane)," 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Sacramento, C.A., U.S.A., Jul. 2006.
Kim, S.J., Lee, Y.S. and Ko, Y.S., "Research Trend and Histories of Rocket Engines using Hydrogen Peroxide and Liquid Methane as Green Propellants," Journal of the Korean Society of Propulsion Engineers, Vol. 14, No. 4, pp. 46-58, 2010.
Pourpoint, T., Meyer, S. and Ehresman,C., "Propulsion Test Facilities at the Purdue University Maurice J.Zucrow Laboratories," 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Cincinnati, O.H., U.S.A., AIAA 2007-5333, Jul. 2007.
Bryner, E., Dyck, D. and Kurtz, C., "Rocket Development and Testing Capabilities at Embry-Riddle Aeronautical University - Prescott AZ campus, "AIAA Propulsion and Energy 2019 Forum, Indianapolis, I.N., U.S.A., AIAA 2019-3892, Aug. 2019.
Bauer, C., Schlieben, G., Eiringhaus, D. and Haidn, O., "Design and commission of a mobile GOX/GCH4 rocket combustion test bed for education and collegiate research," 29th International Symposium Space Technology and Science, Nagoya, Japan, Jun. 2013.
Ommi, F., Mehrabi, A. and Nekoufar, K., "A Practical Scenario for Cold and Hot-Fire Test of a Liquid Subscale Engine with Single Swirl Double Base Injector," International Journal of Engineering & Technology Sciences, Vol. 3, No. 2, pp. 84-100, 2015.
"UBC Rocket", https://vancouversun.com/news/local-news/ubc-engineering-students-aim-for-the-stars-to-go-to-space, retrieved 20 Jan. 2021.
Kim, D.H., Lee, I.C., Kim, J.K., Koo, J.Y. and Park, Y.I, "Performance and Ignition Characteristic of a Coaxial Swirl Injector using LOX-GCH4 Propellant," 35th KSPE Fall Conference, Jeju, Korea, pp. 72-76, Nov. 2010.
"Rocket Prorulsion Combustion Laboratory", http://www.cnurocket.com/main/page.html?pid48, retrieved 14 Dec. 2020.
Kang, C.W., Hwang, D.H., Ahn, J.H, Lee J.S. and Ahn, K.B., "Preliminary Hot-firing Tests of 400 N Class Methane Engine Thrust Chamber," 54th KSPE Spring Conference, Jeju, Korea, KSPE 2020-1086, Jul. 2020.
Huzel, D. K. and Huang, D. H., Modern Engineering for Design of Liquid-Propellant Rocket Engines, Progress in Astronautics and Aeronautics, Washington, D.C., U.S.A., 1992.
Klem, M.D. and Fry, R.S., "Guidelines for Combustion Stability Specifications and Verification Procedures for Liquid Propellant Rocket Engines," CPIA publication 665, 1997.
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