To improve the efficiency of rocket design and prototyping, I developed a MATLAB-based parametric tool to generate rocket nose cone geometries. The code allows the creation of ogive, von Karman, and conical nose cone profiles, enabling rapid modification of geometric parameters such as length, diameter, and shape. The program automatically generates DXF files that can be imported directly into Autodesk Fusion and SolidWorks for CAD modeling and manufacturing preparation. This tool simplifies the transition from analytical design to mechanical modeling, improving efficiency in the rocket aerodynamic design process.
Project Type
MATLAB Code
Location
Irvine, CA, USA
Role/Type
Personal Project
Time
February 2026



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