Liberty University

The meeting served as a technical safety review for the Oklahoma State University rocket team. Key discussion topics included recovery calculations, parachute sizes, airframe construction, fin attachment methods, epoxy and bonding processes, motor retention, and flight readiness preparations. The mentor reviewed the team's Open Rocket simulations, drogue and main deployment parameters, and addressed specific questions regarding fin stability, potential drift, and overall construction quality to ensure compliance with competition standards.

The town hall covered logistical planning for the upcoming competition, including Discord server usage guidelines, certification launch events, and volunteer opportunities. Key topics included registration requirements and deadlines for fun flights and certification attempts, rocket range safety inspection policies, and the requirement for international students to arrive early for certification opportunities. Discussions also addressed shipping coordination for rocket projects, vendor support for equipment, and travel and lodging recommendations. Administrative requirements for team registration and safety reviews were also emphasized.

The discussion focused on the readiness for review of the IREC Team 500 rocket. Key topics included the mechanical design of the booster and sustainer stages, recovery systems, motor retention mechanisms, interstage coupling for ignition, payload structure and experimental goals, and avionics configuration. The team reviewed component specifications, safety factors, flight simulation results, and parachute deployment configurations.

The team conducted a technical review of the rocket design, covering structural components of the nose cone, body tubes, parachute recovery systems, and electronic housing. Key discussions included the materials used for 3D printed parts, battery selection for flight computers and video systems, motor retention methods, and the structural integrity of the air brakes and fins. The team also verified stability simulations for the upcoming IREC launch.

The presentation covered the manufacturing and construction status of the University of Georgia's rocket, including details on structural components, airframe modifications, and motor retention methods. The team discussed their air brake system, which was successfully tested to control apogee, and their payload experiment involving a prosthetic heart valve. Recovery system performance, including dual separation and parachute deployment, was reviewed. The team also discussed avionics, sensor configurations, and flight data analysis, concluding with logistics planning for the upcoming competition.