Acknowledgement
본 연구는 방위사업청 국방과학연구소 기초연구사업(2016-05-044)과 한국항공우주연구원이 지원하는 한국형발사체개발사업(2019M1A3A1A020-9859913)의 지원에 의해 수행되었습니다.
References
- Elverum, G.W., Staudhammer, P. and Miller, J., "The Descent Engine For the Lunar Module," 3rd Propulsion Joint Specialist Conference, Washington, DC., U.S.A., AIAA 1967-521, Jul. 1967.
- Gordon, A.D. and Martin, B., "TRW Pintle Engine Heritage and Performance Characteristics," 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Las Vegas, N.V., U.S.A., AIAA 2000-3871, Jul. 2000.
- Chang, Y., Zou, J., Li, Q. and Cheng, P., "Numerical Study on Combustion and Heat Transfer of a GOX/GCH4 Pintle Injector," 2018 Asia-Pacific International Symposium on Aerospace Technology, Sanghai, China, Jul. 2018.
- Muss, A.J., Johnson, W.C., Kruse W. and Cohn K.R., "The Performance of Hydrocarbon Fuels with H2O2 in a Uni-element Combustor," 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Las Vegas, N.V., U.S.A., AIAA 2003-4623, July. 2003.
- Fang, X. and Shen, C.B., "Study on Atomization and Combustion Characteristics of LOX/methane pintle injectors," Acta Astronautica, Vol. 136, pp. 369-379, 2017. https://doi.org/10.1016/j.actaastro.2017.03.025
- Ryu, H., Yu, I., Kim, W., Shin, D., Ko, Y. and Kim, S., "Experimental Investigation on Combustion Performance of a Pintle Injector Engine with Double-row Rectangular Slot," Journal of the Korean Society of Propulsion Engineers, Vol. 21, No. 3, pp. 25-33, 2017. https://doi.org/10.6108/KSPE.2017.21.3.025
- Nam, J., Lee, K., Park, S., Huh, H. and Koo, J., "Spray Characteristics of a Movable Pintle Injector with Pintle Tip Shape," The Korean Society for Aeronautical and Space Sciences, Vol. 47, No. 9, pp. 658-664, 2019. https://doi.org/10.5139/JKSAS.2019.47.9.658
- Han, D.H., Yoo, Y.L. and Sung, H.G., "An Analysis of the Different Flow Characteristics of a Closed Bomb Test in Cylindrical and Spherical Closed Vessels," International Journal of Aeronautical and Space Sciences, Vol. 20, pp. 150-156, 2018.
- Abramzon, B. and Sirignano, W.A., "Droplet Vaporization Model for Spray Combustion Calculations," International Journal of Heat and Mass Transfer, Vol. 32, No. 9, pp. 1605-1618, 1989. https://doi.org/10.1016/0017-9310(89)90043-4
- Kang, J.S. and Sung, H.G., "Kerosene/GOx Dynamic Combustion Characteristics in a Mixing Layer Under Supercritical Conditions Using the LES-FP approach," Fuel, Vol. 203, pp. 579-590, 2017. https://doi.org/10.1016/j.fuel.2017.04.088
- Shine, S.R., Kumar, S.S. and Suresh, B.N., "A New Generalised Model for Liquid Film Cooling in Rocket Combustion Chambers," International Journal of Heat and Mass Transfer, Vol. 55, pp. 5065-5075, 2012. https://doi.org/10.1016/j.ijheatmasstransfer.2012.05.006
- Yoo, Y.L. and Sung, H.G., "Numerical Investigation of an Interaction Between Shock Waves and Bubble in a Compressible Multiphase Flow Using a Diffuse Interface Method," International Journal of Heat and mass Transfer, Vol. 127, No. 1, pp. 210-221, 2018. https://doi.org/10.1016/j.ijheatmasstransfer.2018.08.012
- Zettervall, N., Fureby, C. and Nilsson, E.J.K., "A Small Skeletal Kinetic Mechanism for Kerosene," Energy & Fuels, Vol. 30, No. 11, pp. 9801-9813, 2016. https://doi.org/10.1021/acs.energyfuels.6b01664
- Strelkova, M.I., Kirillov, I.A., Potapkin, B.V., Safonov, A.A. and Sukhanov, L.P., "Detailed and Reduced Mechanisms of Jet A Combustion at High Temperature," Combustion Science and Technology, Vol. 180, pp. 1788-1802, 2008. https://doi.org/10.1080/00102200802258379
- CHEMKIN-PRO 15512, Reaction Design: San Diego, 2011.
- Turns, S.R., An Introudction to Combustion Conecpts and Application, 3rd ed., Mc Graw Hill, New York, N.Y., U.S.A., 2012
- Morrell, G., "Investigation of Internal Film Cooling of a 1000-pound Thrust Liquid Ammonia Liquid Oxygen Rocket," Technical Report, NACA RME51E04, 1951.