BIOGRAPHY
Dr Jeongmoo Huh is an Assistant Professor in the Department of Mechanical Engineering, United Arab Emirates University(UAEU). He is also an affiliated faculty in the National Space Science and Technology Center(NSSTC) and National Water and Energy Center(NWEC), UAEU. He received his Ph.D. degree in Department of Aerospace Engineering from Korea Advanced Institute of Science and Technology(KAIST), Korea, in Feb 2016.
Before joining the UAEU in Jan 2021, he worked in Korea Institute of Energy Research(KIER), a Korean government-based research centre, doing his Young Scientist Fellowship, participating in a project for Hydrogen Energy and Future Energy Storage Technology. He was a Visiting Researcher at the Department of Space Engineering, Faculty of Aerospace Engineering, Delft University of Technology(TU Delft) in the Netherlands from July 2019 to Feb 2020, and a Postdoctoral Research Assistant at Queen Mary, University of London in the UK from April 2017 to June 2019, participating in the HiperLoc-EP project, a Horizon-2020 scheme project funded by the EU, aiming High-performance Low-cost Disruptive Propulsion Technology Development using Electrospray Colloid Propulsion for small-scale satellite applications.
His research interest includes Green Propulsion, MEMS-based Combustion and Propulsion, Chemical/Electric Propulsion, Sounding Rocket, Photolithography for MEMS fabrication, Energy and Power Conversion Systems, and more.
EDUCATION
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Doctorate Degree, Doctor of Philosophy, Aerospace Engineering, Korea Advanced Institute of Science and Technology, 2016
RESEARCH AREAS
- Power and energy conversion systems
- Aerospace propulsion system
- Chemical space/micro propulsion
- Sounding rocket system
- Electric colloid propulsion
- Novel propellant development
- Photolithography for MEMS fabrication
RECENT PUBLICATIONS
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(2024). "Combustion of Date Stone and Jojoba Solid Waste in a Hybrid Rocket-Like Combustion Chamber". Co-Authors: . Aerospace. 11.
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(2023). "Effect of Structural Materials on Monopropellant Thruster Propulsion Performance in Micro Scale". Co-Authors:
. Aerospace. 10.
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(2022). "Performance of MEMS-Based Monopropellant Microthruster With Insulating Effect". Co-Authors: . Journal of Microelectromechanical Systems. .
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(2022). "A practical design approach for a single-stage sounding rocket to reach a target altitude". Co-Authors: . The Aeronautical Journal. .
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(2021). "Scale-up Potential of Multiport Solid Fuel using Regression Rate Equation in H2O2 Hybrid Rocket". Co-Authors: . Journal of Spacecraft and Rockets . .
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(2021). "Port Diameter Design of Multiport Solid Fuel in Hydrogen Peroxide Hybrid Rockets". Co-Authors: . Aerospace Science and Technology. .
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(2021). "Three-Dimensionally Printed Polylactic Acid as Solid Fuel for Hydrogen Peroxide Hybrid Rockets". Co-Authors: . Journal of Propulsion and Power. .
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(2020). "Integration validation of key components for small sounding rockets". Co-Authors: . Aerospace Science and Technology. .
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(2018). "Preliminary assessment of hydrogen peroxide gel as an oxidizer in a catalyst ignited hybrid thruster". Co-Authors: . International Journal of Aerospace Engineering. .
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(2018). "Effect of Alcohol Carbon Chain on Enthalpy of Combustion and Ignition Delay Time for Gelled Hypergolic Propellant System". Co-Authors: . Propellants Explosives Pyrotechnics. .
