Dynamics Engineer
CurrentWorking on a 5" diameter solid rocket for the 2025 Intercollegiate Rocketry Engineering Competition designed to take a 3U CubeSat payload to 30,000 ft on 21 kN-s of impulse.Characterized shocks and wave drag with Star-CCM+ using approximations from RASAero II for a new varying nose cone tip design.Verified heating and pressures on nose cone tip and fin.