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한국추진공학회지 = Journal of the Korean Society of Propulsion Engineers, v.24 no.6, 2020년, pp.1 - 9
강동혁 (Combustion Chamber Team, Rocket Engine Development Office, Korea Aerospace Research Institute) , 황도근 (Combustion Chamber Team, Rocket Engine Development Office, Korea Aerospace Research Institute) , 유철성 (Combustion Chamber Team, Rocket Engine Development Office, Korea Aerospace Research Institute) , 고영성 (School of Aerospace Engineering, Chungnam National University)
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Using kerosene and liquid oxygen, 1.5-tonf class liquid-liquid pintle injector with rectangular two-row orifice was designed and manufactured. The combustion test of the pintle injector was carried out to verify the combustion performance and combustion stability under a supercritical condition whic...
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Kang, D.H., Hwang, D.H., Lee, B.Y., Kim, J.G., Choi, H.S. and Ko, Y.S., "A study on spray and mixing characteristics of a liquid-liquid pintle injector with the variation of total momentum ratio," 2019 KSPE Fall Conference, Seogwipo-si, Jeju-do, Korea, May 2019.
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