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Past Project
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Development of Flat Air Bearing System for Satellite Cold Gas RCS Controller Testing
Designed and developed a Flat Air Bearing system for testing satellite Reaction Control System (RCS) controllers. The system provided a frictionless testing environment that simulated space conditions for accurate verification of cold gas thruster control systems. Successfully implemented attitude control algorithms and validated their performance through extensive testing on the air bearing platform.
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Development Experience in Marine Debris Cleaning System using UAV-AI-USV Integration
Developed an integrated system combining UAVs (Multicopters), USVs (Catamaran), and AI technology for marine debris cleanup operations. The system utilized AI-powered image processing for debris detection and classification through UAV surveillance. Designed and implemented an autonomous catamaran USV system capable of navigating to identified debris locations and performing collection operations. The project demonstrated successful integration…
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Project experience in rocket landing using Thrust Vector Control(Project ODMSBR)
Developed a landing control algorithm for reusable rocket systems. Designed and implemented an attitude control system using thrust vector control, and optimized control logic for various landing scenarios. Verified the control system performance through groundtesting and implemented a real-time feedback control system to enable stable landing.
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Development Experience of Environmentally Friendly Propellant and Single Thrust Engine through Rocket Club Startup Project
Established the manufacturing environment for HAN (Hydroxylammonium Nitrate), a high-performance monopropellant, and have completed the setup for propellantproduction. The development of a single thrust engine that uses this propellant is currently underway. The ground combustion test environment has been established, and the design of the single thrust engine is complete. The only remaining step is…
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Internship Experience at UZURO TECH Startup, Participating in a Research Project with the Korea Aerospace Research Institute (KARI) on Development of a Plate-Type Thrust Engine and Propellant Delivery System Using HAN-Based Monopropellant for Orbital Debris Removal
As part of the project to develop a propulsion system for deorbiting a 3U CubeSat, the performance of a plate-type propulsion system was to be validated. To achieve this, a ground-based combustion experiment was designed to analyze the combustion characteristics of the plate-type engine. This experiment allowed for an indirect performance verification of the propulsion…
HANul 
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