Our Work
At Othisis Systems, we push the boundaries of student-led aerospace innovation. From high-powered rockets to cutting-edge propulsion systems, our projects are a testament to engineering excellence, teamwork, and relentless curiosity. Explore our journey of designing, testing, and launching the future of space technology.
01
Jericho
December, 2023
Jericho marked our debut in high-powered rocketry, demonstrating our team's capability in design, simulation, and launch execution.
Key Specifications:
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Motor Class: I-Class
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Targeted Apogee: 1 km
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Achieved Apogee: 850.66 m
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Maximum Speed: Mach 0.536
02
MONU v1
April, 2024
MONU v1 was our first L-Class rocket motor, a crucial step in our propulsion research. It was designed with an aluminum casing, graphite nozzle and powered by KNDX propellant. However, the test resulted in failure due to cracks in the graphite nozzle, caused by faulty manufacturing.
03
MONU v2
May, 2024
Monu V2 was the successful iteration of our first solid rocket motor, overcoming the graphite nozzle failure of its predecessor. This milestone validated our design improvements and marked a significant step forward in our propulsion development.
Key Specifications:
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Motor Class: L2000
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Total Impulse: 4000 Ns
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Burn Time: 1.9 seconds
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Casing Material: Aluminum
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Propellant: KNDX
04
FONU
December, 2024
FONU is a custom-built ESP32-based flight computer, designed for real-time data acquisition and control. It features a Finite State Machine (FSM) for precise flight state transitions and pyro-based recovery deployment, alongside LoRa-based telemetry for reliable long-range communication during flight.
Key Specifications:
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Barometric Sensor: BMP180
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IMU Sensor: BMI088
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GPS Module: M10 U-Blox
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Data Logging: SD Card Storage
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Telemetry: RA-02 LoRa
05
SONUS
December, 2024
SONUS, designed as a testbed to validate all our subsystems, incorporated the MONU propulsion system and FONU flight computer. While the target apogee was 2 km, the rocket achieved an impressive 1.83 km. Launched in December 2024, SONUS marked a major milestone, showcasing advancements in avionics, propulsion, and recovery systems.
Key Specifications:
Motor Class: L-Class
Targeted Apogee: 2 km
Achieved Apogee: 1.83 km
Maximum Speed: Mach 0.8