과제정보
본 논문은 교육부의 재원으로 한국연구재단의 지원을 받아 수행된 기초연구사업(NRF-2016R1D1A3B01012622)의 연구결과임.
참고문헌
- Haeseler, D., Mading, C., Gotz, A., Roubinski, V., Khrissanfov, S. and Berejnoy, V., "Recent Developments for Future Launch Vehicle LOx/HC Rocket Engines," 6th International Symposium on Propulsion for Space Transportation of the 21st Century, Versailles, France, AAAF-02-100, May, 2002.
- Haidn, O.J., "Advanced Rocket Engines," Advances on Propulsion Technology for High-Speed Aircraft, pp. 6-1-6-40, 2008.
- Klepikov, I.A., Katorgin, B. I. and Chvanov, V. K., "The new generation of rocket engines, operating by ecologically safe propellant "liquid oxygen and liquefied natural gas(methane)"", Acta Astronautica, Vol. 41, No. 4-10, pp. 209-217, 1997. https://doi.org/10.1016/S0094-5765(98)00076-9
- Vogt, C., Monai, M., Kramer G.J. and Weckhuysen, B. M., "The renaissance of the Sabatier Reaction and its applications on Earth and in space," Nature Catalysis, Vol. 2, No. 3, pp. 188-197, 2019. https://doi.org/10.1038/s41929-019-0244-4
- Lee, K.O., "An Analysis of Launch Vehicle Development Strategy of SpaceX," Journal of the Korean Society of Propulsion Engineers, Vol. 23, No. 6, pp. 72-86, 2019. https://doi.org/10.6108/KSPE.2019.23.6.072
- Melcher, J.C. and Morehead, R.L., "Combustion Stability Characteristics of the Project Morpheus Liquid Oxygen / Liquid Methane Main Engine," 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Cleveland, Ohio, U.S.A., AIAA 2014-3681, July, 2014.
- Boue, Y., Vinet, P., Magniant, S., Motomura, T., Blasi, R. and Dutheil, J.P., "LOX/ methane reusable rocket propulsion at reach with large scale demonstrators tested," Acta Astronautica, Vol. 152, pp. 542-556, 2018. https://doi.org/10.1016/j.actaastro.2018.06.018
- Cheng, S., "Progress in 30 kN LOX/Methane Expander Cycle Engnine," 69th International Astronautical Congress, Bremen, Germany, IAC-18,C4,1,7,x44075, October, 2018.
- Bae, S.H., Hong, J.Y., Kim, H.D. and Kim, J.S., "Combustion Characteristics of Methane-Oxygen Diffusion Flame Formed by Swirl-coaxial Injector," Journal of the Korean Society of Propulsion Engineers, Vol. 21, No. 2, pp. 1-8, 2017.
- Sobel, D.R. and Spadaccini, L.J., "Hydrocarbon Fuel Cooling Technologies for Advanced Propulsion," International Gas Turbine and Aeroengine Congress & Exposition, Houston, Texas, U.S.A., 95-GT-226, June, 1995.