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2. 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. 

3. 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. 

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5. 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. 

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9. 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. 

10. 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. 

11. 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. 

12. 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. 

13. 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. 

14. 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. 

15. 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. 

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17. 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. 

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19. Kim, Y.J., Kim, M.C. and Kim J.S., "Configuration Design, Hot-firing Test and Performance Evaluation of 200 N-Class GCH 4 /LOx Small Rocket Engine (Part I: A Preliminary Design and Test Apparatus)," Journal of the Korean Society of Propulsion Engineers, Vol. 24, No. 1, pp. 1-8, 2020. 

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20. Jeon, J.S., Mim, J.H., Jang, J.H., Ko, Y.S. and Kim, S.J., "Design and Experimental Verification of Uni-Injector Using Gas Methane and Lox as Propellants, "Transactions of the Korean Society of Mechanical Engineers - B, Vol. 37, No. 3, pp. 275-283, 2013. 

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21. 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. 

22. 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. 

23. Kim, M.C., Kim, Y.J. and Kim J.S., "Configuration Design, Hot-firing Test and Performance Evaluation of 200 N-Class GCH4/LOx Small Rocket Engine (Part II: Steady State-mode Ground Hot-firing Test)," Journal of the Korean Society of Propulsion Engineers, Vol. 24, No. 1, pp. 9-16, 2020. 

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24. 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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