Min Son

Min Son

Senior Aerospace Propulsion & Combustion Expert | Lecturer & Researcher
Werner-Heisenberg-Weg 39, 85577, Neubiberg, DE.

About

Highly accomplished aerospace engineer with extensive experience in space propulsion, combustion, and fluid dynamics, leveraging deep expertise in experimental and numerical research to advance cutting-edge technologies. Proven leader in academic instruction and international scientific collaboration, with a strong record of impactful publications and patents. Committed to driving innovation and fostering knowledge exchange within the aerospace and mechanical engineering fields.

Interests

Research Interests

Space Propulsion, Aerospace Engines, Injectors and Sprays, Combustion, Fluid Dynamics, Thermodynamics, Space Mobility, Advanced Mobility.

Work

Universität der Bundeswehr München
|

Lecturer

München, Bavaria, Germany

Summary

Delivering advanced academic instruction in space propulsion, shaping the next generation of aerospace engineers.

Highlights

Delivering comprehensive lectures and practical sessions on Space Propulsion (Raumfahrtantriebe) to advanced engineering students, fostering expertise in cutting-edge aerospace technologies.

Institute of Thermodynamics, Universität der Bundeswehr München
|

Research Associate

München, Bavaria, Germany

Summary

Leading experimental investigations into phase separation of sprays under extreme conditions for the dtec.bw Project (MaST).

Highlights

Led experimental investigations into phase separation of sprays under transcritical and supercritical conditions for the dtec.bw Project (MaST), advancing fundamental understanding of propulsion fluid dynamics.

Designed and constructed a high-pressure and high-temperature testbench, enabling novel experimental setups for extreme condition research.

Implemented advanced optical and laser diagnostics for precise analysis of spray characteristics and combustion phenomena.

Performed rigorous data reduction and conducted comprehensive qualitative and quantitative analyses to derive actionable insights from experimental results, contributing to multiple publications.

German Aerospace Center (DLR) – Institute of Space Propulsion
|

Post-Doctoral Researcher

Lampoldshausen, Baden-Württemberg, Germany

Summary

Executed experimental and numerical research on combustion instability and data analysis for rocket combustors.

Highlights

Conducted experimental and numerical research on injector-driven combustion instability in BKD research rocket combustors, identifying critical parameters for stable operation.

Analyzed extensive data on low-frequency combustion instability from the LUMEN Methane rocket combustor, contributing to design improvements for enhanced reliability and performance.

Collaborated with international teams on propulsion system optimization, contributing to advancements in space propulsion technology.

Korea Aerospace University
|

Post-Doctoral Researcher

Goyang, Gyeonggi-do, Korea (Republic of)

Summary

Contributed to five research projects focused on aerospace propulsion systems, including rocket and gas-turbine engines.

Highlights

Actively participated in 5 distinct research projects focusing on advanced aerospace propulsion systems, including rocket and gas-turbine engines, contributing to project milestones and deliverables.

Conducted experiments and data collection for propulsion system performance analysis, supporting ongoing research initiatives.

Prepared technical reports and presentations summarizing research findings, facilitating knowledge dissemination within the research group.

Korea Aerospace University
|

Lecturer

Goyang, Gyeonggi-do, Korea (Republic of)

Summary

Provided specialized instruction in combustion engineering to aerospace students.

Highlights

Delivered specialized lectures on Combustion principles to aerospace engineering students, enhancing their foundational knowledge in propulsion systems.

Guided students through complex theoretical concepts and practical applications of combustion, preparing them for advanced studies and industry roles.

Volunteer

Advanced Mobility Expert Network (AMExNet)
|

Organizer

Unknown, Unknown, Unknown

Summary

Organizing initiatives for the Advanced Mobility Expert Network, fostering collaboration of academia and industry.

Highlights

Organizes key initiatives and events for AMExNet, promoting knowledge exchange and networking among mobility experts.

Europe-Korea Conference on Science and Technology
|

Session Chair

Unknown, Unknown, Unknown

Summary

Chairing sessions in Mechanical and Aerospace Technology at a prominent international conference.

Highlights

Chairs sessions in Mechanical and Aerospace Technology at the Europe-Korea Conference on Science and Technology, facilitating expert discussions and presentations among international researchers.

Korea Technology Advisory Group (K-TAG) by KIAT
|

Member

Unknown, Unknown, Korea (Republic of)

Summary

Advising on aerospace systems, engineering, and technology for K-TAG.

Highlights

Provides expert advisory services on Aerospace Systems, Engineering, and Technology as a member of the Korea Technology Advisory Group (K-TAG) by KIAT, influencing national technology roadmaps.

European Korean Association of Mechatronics and Aerospace (EKAMA)
|

General Affairs Director

Unknown, Europe, EU

Summary

Managing general affairs for the European Korean Association of Mechatronics and Aerospace.

Highlights

Oversees general affairs for EKAMA, facilitating operational efficiency and member engagement across European and Korean scientific communities.

Korean Scientists and Engineers Association in Germany (VeKNI e.V.)
|

Leader of Mechanical Engineering Group

Unknown, Germany, Germany

Summary

Leading the Mechanical Engineering Group and organizing events for 220 members.

Highlights

Leads the Mechanical Engineering Group for VeKNI e.V., organizing workshops and seminars for 220 members to foster professional development and networking.

Korea-EU Research Centre (KERC)
|

Member of Supporters

Unknown, Europe, EU

Summary

Contributing to the dissemination of EU aerospace research and policy trends.

Highlights

Publishes EU trend reports on research and policies in the aerospace field, informing strategic discussions and fostering international collaboration.

Europe-Korea Conference on Science and Technology 2023 (EKC 2023)
|

Local Committee Member

Unknown, Unknown, Unknown

Summary

Served as a Local Committee Member for the EKC 2023, supporting an event that attracted approximately 800 participants.

Highlights

Contributed as a Local Committee Member for the Europe-Korea Conference on Science and Technology 2023 (EKC 2023), successfully supporting an event that attracted approximately 800 participants.

Education

Universität der Bundeswehr München
München, Bavaria, Germany

Habilitation

Thermodynamics

Korea Aerospace University
Goyang, Gyeonggi-do, Korea (Republic of)

Ph.D.

Aerospace and Mechanical Engineering

Courses

Dissertation: Correlations between Spray and Combustion Characteristics of a Movable Pintle Injector for Liquid Rocket Engines

Korea Aerospace University
Goyang, Gyeonggi-do, Korea (Republic of)

M.E.

Aerospace and Mechanical Engineering

Courses

Thesis: Optimal Design Methods for Regenerative-cooled Combustor and Fuel-rich Gas-generator of Liquid Rocket Engine

Korea Aerospace University
Goyang, Gyeonggi-do, Korea (Republic of)

B.E.

Aerospace and Mechanical Engineering

Projects

Experimental Investigation on Phase Separation of Sprays in Trans- and Super-critical Conditions (dtec.bw Project MaST)

Summary

Experimental investigation focused on the phase separation of sprays under transcritical and supercritical conditions.

Experimental Investigation of Combustion Instabilities in Liquid Propellant Rocket Engine

Summary

Post-doctoral research at DLR investigating combustion instabilities in liquid propellant rocket engines induced by fluid-mechanical driving sources in the primary injector.

Development of a Low Emission Combustor for 25kN Aero Gas Turbine

Summary

Contribution to the Aerospace Parts and Technology Development Program for a 25kN aero gas turbine combustor.

Suppression Technique of Transverse Disturbance Propagation in Liquid Rocket Combustor

Summary

Research under the Space Core Technology Development Program on using fluidic baffles to suppress transverse disturbance propagation in liquid rocket combustors.

Phase Change and Jet Breakup of Heterogeneous Hydrocarbon Mixture in Supercritical Environment

Summary

Basic Science Research Program focused on the phase change and jet breakup characteristics of heterogeneous hydrocarbon mixtures in supercritical environments.

Spray and Combustion Characteristics of a Pintle Injector for Variable Thrust Rocket

Summary

Research at the Advanced Space Propulsion Research Center on the spray and combustion characteristics of pintle injectors for variable thrust rockets.

Combustion of Gas-Liquid Propellants in Supercritical Conditions

Summary

Research under the Space Core Technology Development Program on the combustion of gas-liquid propellants in supercritical conditions.

An Experimental Research on Internal Flow of Solid Rocket Motor

Summary

Experimental research focusing on the internal flow dynamics of solid rocket motors.

Experimental Study on Pulse Detonation Engines (NRF-RFBR Joint Research Program)

Summary

Experimental study on pulse detonation engines as part of the NRF(Korea)-RFBR(Russia) Joint Research Program, focusing on fundamentals of modern thrust generators.

Publications

Deconvolution of Infrared Spray Images using Optical Depth from Shadowgraphy

Published by

12th European Combustion Meeting

Summary

Presented methods for deconvoluting infrared spray images using optical depth from shadowgraphy.

Application of Artificial Neural Networks to Model Macroscopic Spray Characteristics of Alcohol Fuels

Published by

Engineering Applications of Artificial Intelligence

Summary

Applied artificial neural networks to model macroscopic spray characteristics of alcohol fuels.

Hysteresis-Induced Onset and Progressive Decay of Periodic and Metastable Sheet Cavitation in a Chamfered Circular Orifice

Published by

Fluids

Summary

Explored the onset and decay of sheet cavitation in a circular orifice, focusing on hysteresis effects.

Experimental and Numerical Investigation of Cyclopentane Sprays in Transcritical Environment

Published by

Atomization and Sprays

Summary

Investigated the behavior of cyclopentane sprays under transcritical conditions through experimental and numerical methods.

Microscopic Observation of Fuel Droplet Phase Change in High-Pressure and High-Temperature Environments

Published by

Thermodynamik-Kolloquium 2024

Summary

Presented microscopic observations of fuel droplet phase changes in extreme high-pressure and high-temperature environments.

Macroscopic Fuel Spray Characteristics at Sub/Transcritical Injection Conditions

Published by

31. Fachtagung "Experimentelle Strömungsmechanik"

Summary

Discussed macroscopic fuel spray characteristics under sub/transcritical injection conditions.

Environmental Impact of Rocket Launches in New Space Era

Published by

Europe-Korea Conference on Science and Technology 2024

Summary

Discussed the environmental impact of rocket launches in the context of the new space era.

Dynamic Spectral Analysis of Transcritical Sprays

Published by

Europe-Korea Conference on Science and Technology 2024

Summary

Presented dynamic spectral analysis techniques for transcritical sprays.

Near-critical Phase Changes of Cyclopentane Droplets in Supercritical Nitrogen Environment

Published by

The Combustion Institute's 40th International Symposium

Summary

Presented findings on near-critical phase changes of cyclopentane droplets in a supercritical nitrogen environment.

Integrated Optical Diagnostics of Cyclopentane Sprays to Characterize Transcritical Phase Transitions

Published by

21st International Symposium on Application of Laser and Imaging Techniques to Fluid Mechanics

Summary

Discussed integrated optical diagnostics for characterizing transcritical phase transitions in cyclopentane sprays.

Comparison of Imaging Methods for Transcritical Sprays

Published by

31. Deutscher Flammentag für nachhaltige Verbrennung

Summary

Compared various imaging methods for analyzing transcritical sprays.

Experimental and Numerical Investigation of Cyclopentane Sprays in Transcritical Environment

Published by

ILASS Europe 2023, 32nd Conference on Liquid Atomization & Spray Systems

Summary

Presented experimental and numerical investigations of cyclopentane sprays in a transcritical environment.

Application of Machine Learning Approaches to Model the Temporal Evolution of Fuel Sprays

Published by

ILASS Europe 2023, 32nd Conference on Liquid Atomization & Spray Systems

Summary

Demonstrated the application of machine learning approaches to model the temporal evolution of fuel sprays.

Phase Change Characteristics of Cyclopentane Droplets at Near-critical Conditions

Published by

Europe-Korea Conference on Science and Technology 2023

Summary

Discussed phase change characteristics of cyclopentane droplets at near-critical conditions.

Optical Characterization of Sub- and Transcritical Fuel Sprays using Shadowgraphy, Mie-scattering and Infrared Radiation Measurements

Published by

11th European Combustion Meeting (ECM 2023)

Summary

Presented optical characterization methods for sub- and transcritical fuel sprays using various imaging techniques.

Experimental and modeling analysis of the transient spray characteristics of cyclopentane at sub-and transcritical conditions using a machine learning approach

Published by

Physics of Fluids

Summary

Conducted experimental and modeling analysis of transient cyclopentane spray characteristics using machine learning.

Orifice Flow Dynamics in a Rocket Injector as an Excitation Source of Injector-Driven Combustion Instabilities

Published by

Aerospace

Summary

Analyzed how orifice flow dynamics in rocket injectors contribute to combustion instabilities.

Injection-coupling instabilities in the BKD combustor: Acoustic analysis of the isolated injectors

Published by

AIAA Journal

Summary

Performed acoustic analysis of isolated injectors to understand injection-coupling instabilities in the BKD combustor.

Investigation of sub- and transcritical fuel spray processes using shadowgraphy, Mie scattering and infrared radiation measurements

Published by

Thermodynamik-Kolloquium 2022

Summary

Detailed investigations of sub- and transcritical fuel spray processes using advanced measurement techniques.

Spectral Analysis of Multi-dimensional Periodic Data: Application to Rocket Combustion Instability

Published by

Europe-Korea Conference on Science and Technology 2022

Summary

Applied spectral analysis to multi-dimensional periodic data for understanding rocket combustion instability.

Optical Diagnostics for Fuel Sprays in a High-Pressure and High-Temperature Chamber

Published by

Europe-Korea Conference on Science and Technology 2022

Summary

Presented optical diagnostics techniques for fuel sprays in high-pressure and high-temperature chambers.

Visualization of cavitation and periodical flow fluctuations from a rocket injector orifice

Published by

19th International Symposium on Flow Visualization (ISFV-19)

Summary

Presented visualizations of cavitation and periodical flow fluctuations originating from a rocket injector orifice.

Experimental study of intra-injector flow fluctuations induced by a LOX injector orifice driving combustion instability

Published by

Symposium on Thermoacoustics in Combustion: Industry meets Academia (SoTiC 2020)

Summary

Conducted an experimental study on intra-injector flow fluctuations induced by a LOX injector orifice driving combustion instability.

Numerical study of acoustic resonance in a LOX injector post induced by orifice flow

Published by

AIAA Propulsion and Energy 2021 Forum

Summary

Performed a numerical study on acoustic resonance in a LOX injector post induced by orifice flow.

Velocimetry of a LOX jet in a high-pressure combustion field from high-speed flame images

Published by

ODAS(ONERA-DLR Aerospace Symposium)-MOTAR(Measurement and Optical Techniques for Aerospace Research) 2021

Summary

Presented velocimetry measurements of a LOX jet in a high-pressure combustion field using high-speed flame images.

Characterisation of acoustically coupled flow field dynamics from high-speed imaging in a high pressure rocket thrust chamber

Published by

1st Aerospace Europe Conference (AEC2020)

Summary

Characterized acoustically coupled flow field dynamics using high-speed imaging in high-pressure rocket thrust chambers.

Combustion stability characteristics of a sub-scale LOX/LNG rocket thrust chamber

Published by

1st Aerospace Europe Conference (AEC2020)

Summary

Analyzed combustion stability characteristics of sub-scale LOX/LNG rocket thrust chambers.

Measuring the velocity field of a shear-coaxial, cryogenic flame in a high-pressure rocket thrust chamber

Published by

38th International Symposium on Combustion 2020

Summary

Detailed the measurement of velocity fields in shear-coaxial, cryogenic flames within high-pressure rocket thrust chambers.

Measuring the velocity field of a shear-coaxial, cryogenic flame in a high-pressure rocket thrust chamber

Published by

Proceedings of the Combustion Institute

Summary

Detailed the measurement of velocity fields in cryogenic flames within high-pressure rocket thrust chambers.

Characteristics of anchoring locations and angles for GOX/GCH4 flames of an annular pintle injector

Published by

Acta Astronautica

Summary

Examined the anchoring characteristics of GOX/GCH4 flames in annular pintle injectors.

Flow visualization of cryogenic spray from a movable pintle injector

Published by

Journal of Visualization

Summary

Visualized cryogenic spray behavior from a movable pintle injector.

Flame Structure of Gaseous Methane/Oxygen in a Pintle Injector

Published by

11th International Symposium on Special Topics in Chemical Propulsion & Energetic Materials 2018

Summary

Presented on the flame structure of gaseous methane/oxygen in a pintle injector.

Lagrangian Approach to Axisymmetric Spray Simulation of Pintle Injector for Liquid Rocket Engines

Published by

Atomization and Sprays

Summary

Developed a Lagrangian approach for axisymmetric spray simulation of pintle injectors in liquid rocket engines.

Effects of nitrogen film cooling on ignition transition of gaseous oxygen/kerosene spray combustor

Published by

Combustion Science and Technology

Summary

Studied the effects of nitrogen film cooling on ignition transition in gaseous oxygen/kerosene spray combustors.

Effect of Injection Conditions on Mixing Performance of Pintle Injector for Liquid Rocket Engines

Published by

Acta Astronautica

Summary

Investigated the impact of injection conditions on the mixing performance of pintle injectors in liquid rocket engines.

Effects of Supercritical Environment on Hydrocarbon-fuel Injection

Published by

Journal of Thermal Science

Summary

Analyzed the effects of a supercritical environment on hydrocarbon-fuel injection processes.

Design Procedure of a Movable Pintle Injector for Liquid Rocket Engines

Published by

Journal of Propulsion and Power

Summary

Outlined a design procedure for movable pintle injectors used in liquid rocket engines.

Numerical study on the combustion characteristics of a fuel-centered pintle injector for methane rocket engines

Published by

Acta Astronautica

Summary

Conducted a numerical study on combustion characteristics of fuel-centered pintle injectors for methane rocket engines.

Reliability Study on Skewness of Doublet Impinging Injectors

Published by

Journal of Mechanical Science and Technology

Summary

Conducted a reliability study on the skewness of doublet impinging injectors.

Verification on spray simulation of a pintle injector for liquid rocket engine

Published by

Journal of Thermal Science

Summary

Verified spray simulation models for pintle injectors in liquid rocket engines.

Numerical Study on the Combustion Characteristics of a Fuel-centered Pintle Injector for Methane Rocket Engines

Published by

Third IAA Symposium of Space Flight Safety 2016

Summary

Conducted a numerical study on the combustion characteristics of fuel-centered pintle injectors for methane rocket engines.

GCH4-Air Flame Characteristics of a Pintle Injector Designed for Liquid Rocket Engines in Atmospheric Condition

Published by

8th Asian Joint Conference on Propulsion and Power 2016

Summary

Investigated GCH4-air flame characteristics of a pintle injector designed for liquid rocket engines under atmospheric conditions.

Design Procedure of a Movable Pintle Injector for Liquid Rocket Engines

Published by

54th AIAA Aerospace Sciences Meeting 2016

Summary

Presented a design procedure for movable pintle injectors for liquid rocket engines.

Ignition Transition of Coaxial Kerosene/Gaseous Oxygen Jet

Published by

Combustion Science and Technology

Summary

Investigated the ignition transition of coaxial kerosene/gaseous oxygen jets.

Verification on Spray Simulation of a Pintle Injector for Liquid Rocket Engine

Published by

12th International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows 2015

Summary

Presented verification of spray simulation for pintle injectors in liquid rocket engines.

Cone Angle Characteristics of Pintle Injector spray at Atmospheric Condition

Published by

8th Asian-Pacific Conference on Aerospace Technology and Science 2015

Summary

Analyzed cone angle characteristics of pintle injector sprays under atmospheric conditions.

Effects of Momentum Ratio and Weber Number on Spray Half Angles of Liquid Controlled Pintle Injector

Published by

Journal of Thermal Science

Summary

Investigated the impact of momentum ratio and Weber number on spray half angles in liquid-controlled pintle injectors.

Reliability Study on Spray Performances of a Pintle Injector for Liquid Rocket Engines based on Sensitivity Analysis

Published by

3rd International Conference on Materials and Reliability 2015

Summary

Conducted a reliability study on the spray performances of pintle injectors for liquid rocket engines using sensitivity analysis.

Development of a Moveable Sleeve Injector with a Fixed Pintle for a Throttleable Rocket Combustor

Published by

66th International Astronautical Congress 2015

Summary

Developed a movable sleeve injector with a fixed pintle for throttleable rocket combustors.

Design optimization of a methane-fuel rocket combustor with a genetic algorithm

Published by

Journal of Mechanical Science and Technology

Summary

Optimized the design of a methane-fuel rocket combustor using a genetic algorithm.

Effects of Pintle-tip Angles on Spray Characteristics of Movable Pintle Injector

Published by

13th International Conference on Liquid Atomization and Spray Systems 2015

Summary

Investigated the effects of pintle-tip angles on spray characteristics of movable pintle injectors.

Flow Disturbance Characteristics on Fin-slot Shaped Grain Simulator of Solid Rocket Motor with Submerged Nozzle

Published by

Space Propulsion 2014

Summary

Analyzed flow disturbance characteristics on a fin-slot shaped grain simulator of a solid rocket motor with a submerged nozzle.

Liquid Jets Breakup and Mixing Characteristics from a Pintle Injector

Published by

26th European Conference on Liquid Atomization and Spray Systems 2014

Summary

Investigated liquid jet breakup and mixing characteristics from a pintle injector.

Atomization and Combustion Characteristics of Ethanol/Nitrous Oxide at Various Momentum Flux Ratios

Published by

Energy & Fuels

Summary

Studied atomization and combustion characteristics of ethanol/nitrous oxide at varying momentum flux ratios.

Genetic Algorithm to Optimize the Design of Main Combustor and Gas Generator in Liquid Rocket Engines

Published by

Journal of Thermal Science

Summary

Applied genetic algorithms to optimize the design of main combustors and gas generators in liquid rocket engines.

Design Optimization of Methane-fuel Rocket Combustor with Genetic Algorithm

Published by

8th China-Japan-Korea Joint Symposium on Optimization of Structural and Mechanical Systems 2014

Summary

Optimized the design of a methane-fuel rocket combustor using a genetic algorithm.

Liquid Sheet Breakup by Gas Jet Injected from Pintle Injector

Published by

5th Asian Joint Workshop on Thermophysics and Fluid Science 2014

Summary

Studied liquid sheet breakup caused by gas jet injection from a pintle injector.

Detonation Characteristics of Acetylene-oxygen with Additional Liquid Fuel

Published by

21st International Symposium on Air Breathing Engines Conference 2013

Summary

Investigated the detonation characteristics of acetylene-oxygen with additional liquid fuel.

Fundamental Study on Detonation Wave Characteristics of Acetylene-Oxygen Mixture for Pulse Detonation Engine

Published by

24th International Colloquium on the Dynamics of Explosions and Reactive Systems 2013

Summary

Conducted a fundamental study on detonation wave characteristics of acetylene-oxygen mixtures for pulse detonation engines.

Development of Design Methods for Kerosene Fuel-rich Gas-generator and Preburner

Published by

Asian Joint Conference on Propulsion and Power 2012

Summary

Developed design methods for kerosene fuel-rich gas-generators and preburners.

Computational Design Method for Main Combustor Profile and Regenerative Cooling Channel Shape of Liquid Rocket Engine

Published by

2nd International Conference on Computational Design in Engineering 2012

Summary

Developed a computational design method for the main combustor profile and regenerative cooling channel shape of liquid rocket engines.

Experimental Study on Detonation Characteristics of Acetylene and Oxygen Mixture

Published by

Hong Kong International Conference on Engineering and Applied Science 2012

Summary

Conducted an experimental study on detonation characteristics of acetylene and oxygen mixtures.

Conceptual Design for a Kerosene Fuel-rich Gas-generator of a Turbopump-fed Liquid Rocket Engine

Published by

Journal of Thermal Science

Summary

Developed a conceptual design for a kerosene fuel-rich gas-generator for turbopump-fed liquid rocket engines.

Development of Preliminary Design Program for Combustor of Regenerative Cooled Liquid Rocket Engine

Published by

Journal of Thermal Science

Summary

Developed a preliminary design program for regenerative-cooled liquid rocket engine combustors.