[작성자:] Hanul CU

  • Recent Activities ⭐️

    Recent Achievements for the 2025 IREC 2025.05.02 ‘Project Technical Reports & Presentations’ submitted 2025.04.12 Yuri’s night Korea in DAEJEON We participated in Yuri’s Night, a global event celebrating the first human in space! 🚀Yuri’s Night is held every year around the world to honor Yuri Gagarin’s historic spaceflight on April 12, 1961. 🌍🌌 By running

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  • Structure

    Structure

    Airframe Diameter (mm) Number of fins 136.0 8

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  • 2024 KSPE Fall Conference

    2024 KSPE Fall Conference

    We participated in the 2024 KSPE Fall Conference held at Paradise Hotel Busan from November 27th to 29th, 2024! 🚀 During the conference, we attended various presentations, participated in exhibition booths, and had valuable opportunities to connect with companies. It was an enriching experience to learn about new technologies and network with experts in the

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  • Other Outreach

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  • Past project

    Click the title and see more information! Past Project

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  • Academic

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  • TEST

    TEST

    Key Test Objectives 1. RCS Control System 2. Sensor & Data Systems 3. Recovery Systems 4. Emergency Procedures Key Test Objectives

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  • Recovery

    Recovery

    In our recovery system, the drogue parachute is deployed at apogee. The secondary charge is activated 1 second after apogee. The main parachute is deployed at an altitude of 1,000 feet, and its secondary charge is also triggered 1 second after reaching that altitude. The parachute diameters are 2.3 feet for the drogue and 7.22

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  • Electronics

    Electronics

    1. COTS Flight Computers Primary Recovery System: Tracking System Data Collection 2. SRAD Flight Computer Main Processing Units Sensor Array 3. RCS (Reaction Control System) Components Solenoid Valve System Control System 4. Communication Systems Telemetry System Real-time Video Processing 5. Data Storage and Management Storage Solutions Data Management 6. Power Management Power Distribution 7. Ground

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  • Payload

    Payload

    The payload in this project adheres to the 3U CubeSAT standard and includes three advanced IMU sensors (10-DoF MEMS IMU sensor [SEN0140], 9DOF IMU AHRS sensor module, and 9-axis IMU LSM9DS1 module) to measure vibration, acceleration, and angular velocity, aiming to validate sensor durability and vibration resistance under launch conditions, comparing data over altitude and

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