Rocket Propulsion Lab – Daedalus
Student-built rocket structures, aerodynamic trades, and test instrumentation
Worked within UCSD Rocket Propulsion Lab to design and validate structural components for a student-built rocket targeting a 4,000-ft apogee. The work combined structural design, aerodynamic trade studies, and integrated validation across propulsion and recovery interfaces.
- Balancing structural rigidity with weight constraints so the vehicle remained robust without driving unnecessary mass growth.
- Maintaining a stable aerodynamic configuration while accounting for drag, stability margin, and mass distribution shifts.
- Integrating structural components cleanly with propulsion and recovery systems without creating assembly or test bottlenecks.
- Supported propulsion and recovery validation with structured instrumentation and data collection during subsystem testing.
- Compared predicted aerodynamic behavior against measured configuration changes to guide iteration before integration.
- Established a more defensible structural design process linking CAD, FEA, and aerodynamic analysis.