International Rocket Engineering Competition Project

The Structures team is responsible for designing and testing all airframe components for the rocket. The team focuses on the research and development of airframes, fins, nose cones, and any specialty aerodynamic components. They also conduct structural tests to verify manufacturing techniques and airframe design.

The Avionics team is responsible for designing, testing, and manufacturing all flight computers, sensors, and telemetry systems and ensuring that rocket recovery systems are functional. Avionics works closely with all teams to collect proper data for a successful flight. Additionally, they work closely with Recovery and Payload to assist and ensure the proper systems and data collection systems work for their needs.

The Aerodynamics team focuses on evaluating the performance of the rocket during flight. Recently the team has been analyzing the effects of the transition piece in the middle of the rocket in addition to the nose cone shape. Work includes consulting aerodynamic literature and using Ansys Fluent to run Computational Fluid Dynamics simulations.

The Payload team focuses on designing a payload that conforms to the competition requirements. The Payload team works to have multiple experiments onboard, including a team concept and an outreach project working with local organizations in Columbus, OH. Work includes experiment brainstorming, design, development, and analysis post-flight.

The Propulsion team researches and develops a solid propellant rocket motor. Work includes creating a custom propellant formula, utilizing solid motor fabrication techniques, conducting motor hot fire tests to verify design, and integration to launch vehicle.