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Airflow test of the 2024 diffuser prototype

Retesting the fins at 10 degrees of Angle of Attack

Continuing the integration of grid fin testing for force moments at various AOA.

Component of researching the grid fin design on reusable rockets over various AOA

Cálculo del coeficiente de arrastre de un cono a altas velocidades

Testing the control model of a reusable rocket.

This project is a demonstration of conjugate heat transfer analysis of a directional vane disk, a critical component of a disk brake system. The primary objective of the study is to investigate the heat dissipation characteristics of the disk under the influence of airflow.

The analysis is grounded in thermo-fluid dynamics, integrating principles of both thermodynamics and fluid mechanics to simulate real-world conditions. The project employs a conjugate heat transfer approach, which allows for the simultaneous examination of heat transfer due to conduction, convection, and radiation. This methodology provides a holistic understanding of the thermal behavior of the disk brake system. A rotating zone is also added to account for the rotational effects of the disk.

The directional vane disk, with its unique design and material properties, plays a pivotal role in the heat dissipation process. The project aims to study the influence of airflow on this process, considering factors such as airflow velocity, direction, and ambient temperature.

Testing the final degree tilt for modified SpaceX Grid Fin

Testing a novel lattice fin for torque moment on reusable rocket

The project goal is to conduct a simulation of the internal dynamics within a current transformer during an internal arcing event.

Analyser la propagation de chaleur dans le boitier électronique de l'appareil afin de déterminer l'aération nécessaire au bon refroidissement de la carte électronique qui s'y trouve

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