Home

Featured Project

Pneumatic Launchers

Exploring the physics and engineering of high-velocity pneumatic systems. All demonstrations conducted legally in Hong Kong.

Theoretical Design

Boba Launcher — Version 2

Boba CAD

CAD Design

Developed a detailed SolidWorks model exploring pressure chamber geometry, sealing strategies, and projectile guidance under a 70 psi maximum operating pressure constraint while achieving a theoretical launch velocity of 50 m/s.

The design uses only real off-the-shelf, pressure-rated PVC standards and commercially available solenoid valves, rather than custom components. This constraint strongly influenced geometry, layout, and structural decisions. The project remains a theoretical design.

ANSYS Simulation

ANSYS Simulation

Structural integrity was evaluated using static load analysis in ANSYS Mechanical to verify stress distributions under theoretical internal pressure loads. Internal flow behavior was studied using ANSYS Fluent to estimate theoretical performance and velocity trends.

These simulations served as comparative design tools to understand system behavior and tradeoffs rather than optimizing for construction.

Design Models

Model 1 Model 2 Model 3

Practical Implementation

Putty Launcher — Version 1

Adiabatic Calculations

Adiabatic Calculations

This project launched a 15 g putty projectile at approximately 40–50 m/s using a maximum operating pressure of 50 psi.

Theoretical performance modeling was based on adiabatic expansion of a diatomic gas, justified by experimental pressure measurements indicating characteristic expansion times of 75–150 ms. This allowed closed-form energy and pressure relationships to be derived.

View Full Report (PDF)
Testing

CAD + Testing + Prototypes

Modeled the full assembly in CAD and performed basic validation of mechanical loading assumptions. Iterated on barrel geometry, chamber volume, and layout to improve consistency and repeatability with readily available components. Additionally performed static pressure tests for safety assurance.

Final Product

Final Product Showcase

The final system demonstrated consistent performance across repeated tests. Design iteration focused on improving valve response consistency, sealing reliability, and projectile–barrel interface behavior. Testing was conducted on secured private property in Hong Kong in accordance with local legal constraints.

Launch Demonstrations

Conducted legally in Hong Kong