Prototype 1

Our prototype sought out to be a physical compilation, containing main subsystems like the housing capsule, rocket body, and Flight Computer to actualize dimensions and fitment to eventually perform a test launch on 13 December 2025. This was to answer the question: What are the appropriate dimensions needed to adequately fit all of the housing components? Below are photos of the subsystems worked on during this prototype phase.

Flight Computer

Housing Capsule

Prototype 1 Assembly All Parts

These components were then fitted into the first assembly of the rocket body. With fitment being a success, the plan moving forward for future iterations is improving the sensor implementation of the Flight Computer, utilizing more fin simulation within RockSim and FEA software analysis for our future launch.

Prototype 2

Our prototype again sought out to secure proper fitment of all manufactured parts and ensure systems operate properly through testing through printing more parts. This was to answer the question: How do our parts in SolidWorks translate to real life models? Below are photos of the subsystems worked on during this prototype phase.

Control Mechanisms Assembled

Control Mechanisms (SolidWorks)

Ring

Fuselage

These components were then fitted to the second iteration of the rocket body assembly. However, we learned that because of the complex geomtry of our parts, some of them were not functioning as intended. For the next iteration, the fuselage's diameter will be changed to 3 in. in fiberglass, the rings will have to be reprinted due to a thickness error, and the control system will involve bigger connecting pieces for easier assembly.

Prototype 1

Prototype 2

CAD Drawings