Personal profile
In Korean
이정표 교수(공과대학 기계공학부)
Education
o (1998) B.A., Korea Aerospace University, Goyang, Korea
o (2005) M.A., Korea Aerospace University, Goyang, Korea
o (2013) Ph.D, Korea Aerospace University, Goyang, Korea
o (2005) M.A., Korea Aerospace University, Goyang, Korea
o (2013) Ph.D, Korea Aerospace University, Goyang, Korea
Professional Experience
o (2017~2024) Associate Professor, University of Brasilia, Brazil
o (2015~2017) Assistant Professor, University of Brasilia, Brazil
o (2020~2021, 2011~2012) Adjunct Professor/Lecturer at Korea Aerospace University
o (2019, 2023) Editorial Board Member, The Korean Society of Propulsion Engineers (KSPE)
o (2023) External Director, INNOSPACE Co., Ltd, Sejong-si
o (2020~2021) Chief Researcher, INNOSPACE Co., Ltd, Sejong-si
o (2014~2015) Postdoctoral Fellow, University of Brasilia, Brazil
o (2015~2017) Assistant Professor, University of Brasilia, Brazil
o (2020~2021, 2011~2012) Adjunct Professor/Lecturer at Korea Aerospace University
o (2019, 2023) Editorial Board Member, The Korean Society of Propulsion Engineers (KSPE)
o (2023) External Director, INNOSPACE Co., Ltd, Sejong-si
o (2020~2021) Chief Researcher, INNOSPACE Co., Ltd, Sejong-si
o (2014~2015) Postdoctoral Fellow, University of Brasilia, Brazil
Research Interests
o Rocket Propulsion
o Internal ballistics analysis
o Fluid-dynamics, Thermodynamics, Heat transfer
o Combustion instability
o Solid Fuel Ramjet
o Sounding Rocket System Integration
o Internal ballistics analysis
o Fluid-dynamics, Thermodynamics, Heat transfer
o Combustion instability
o Solid Fuel Ramjet
o Sounding Rocket System Integration
Major Research Achievements
o Thermal–Combustion Coupled Instability in Hybrid Rockets with Fuel Blowing
o Combustion Instability Mechanism in Hybrid Rocket Motors with Diaphragm
o Experimental and Numerical Study of the Flammability Limits in a CH4/O2 Torch Ignition System
o Development and Performance Analysis of Gas Generator with Plunger-type Flow Control Valve for Ducted Rocket
o Role of Precombustion Chamber Design in Feed-System Coupled Instabilities of Hybrid Rockets
o Combustion Instability Mechanism in Hybrid Rocket Motors with Diaphragm
o Experimental and Numerical Study of the Flammability Limits in a CH4/O2 Torch Ignition System
o Development and Performance Analysis of Gas Generator with Plunger-type Flow Control Valve for Ducted Rocket
o Role of Precombustion Chamber Design in Feed-System Coupled Instabilities of Hybrid Rockets
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Collaborations and top research areas from the last five years
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Analytical and Numerical Determination of Acoustic Modes of 25 kN Liquid Propellant Rocket Engine
Gontijo, M. S. Á., Sant’Ana, M. S., Yamada, P. Y., Filho, R. D. B. D. N., Schrammel, A. J., Shynkarenko, O., Lee, J. & Bertoldi, A. E. D. M., 2025, Advances in Aerospace Sciences - Selected Papers from COBEM 2023. Souza, D. S., Halila, G. L. O. & Wolf, W. R. (eds.). Springer Science and Business Media Deutschland GmbH, p. 106-119 14 p. (Lecture Notes in Mechanical Engineering).Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review
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AI and Classical Approaches to Estimating Solid Fuel Regression Rate in Hybrid Rocket Engines
Metre Resende, G., Bertoldi, A. E. M., Shynkarenko, O. & Lee, J., 2024, 22nd IAA Symposium on Space Debris - Held at the 75th International Astronautical Congress, IAC 2024. International Astronautical Federation, IAF, p. 1746-1751 6 p. (Proceedings of the International Astronautical Congress, IAC; vol. 3).Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review
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Conceptual design of a 1 kN hybrid rocket engine manufactured with additive technology
Shynkarenko, O., Veras, C. A. G., Lee, J., Bertoldi, A. E. M., Unternbaumen, E., Capparelli, G. & García, H., 2024, 22nd IAA Symposium on Space Debris - Held at the 75th International Astronautical Congress, IAC 2024. International Astronautical Federation, IAF, p. 1682-1696 15 p. (Proceedings of the International Astronautical Congress, IAC; vol. 3).Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review
1 Scopus citations -
Effect of swirl intensity variation on combustion characteristics in end-burning hybrid rocket engines
Lee, J., Woo, K. & Kim, S., Apr 2024, In: Acta Astronautica. 217, p. 302-311 10 p.Research output: Contribution to journal › Article › peer-review
7 Scopus citations -
Thermal-Combustion Coupled Instability in Hybrid Rockets with Fuel Blowing
Lee, J., Moon, H. & Kim, J., May 2023, In: Journal of Propulsion and Power. 39, 3, p. 308-317 10 p.Research output: Contribution to journal › Article › peer-review
1 Scopus citations