This Project was apart of my University Honors Capstone which was in addition to my Senior Capstone for the College of Engineering.
For this project, I designed and built a Level 3 rocket to gain my Level 3 High-powered Rocket Certification. The certification process involved designing a rocket that can fly on an M impulse motor (5120 N*S and above) and successfully recover the airframe.
During the design process, I had to consider aerodynamic performance, thrust loads from the motor, manufacturability of the design, design safety, and recovery systems. Before construction could begin on the rocket, I had to go through several rounds of engineering reviews by Technical Advisory Panel (TAP) members. These TAP members have over 15 years of experience in engineering and high-powered rocket design.
RASAero was used as the primary flight simulation software. The graph shown to the left shows the flight data recorded by an onboard flight computer and the predicted flight profile. The difference in achieved altitude and predicted altitude was about 150 ft.