Document
Dynamics and design calculations

A three-degree-of-freedom launch mechanism developed through multibody dynamics, structural checks, detailed design and physical testing

I rebuilt the mechanism as a three-degree-of-freedom model with one rigid main arm, a floating counterweight link and a massless tension-only sling. The Python simulation integrates the power stroke, selects a feasible release state and switches the projectile to a quadratic-drag flight model.
With the documented mass assumptions, the model predicts a 30.5 m/s release and 43.5 m of range. The report states each estimated component mass so measured or CAD-derived values can replace it.
Recovered joint reactions replace the earlier scalar acceleration estimate. The model gives a 625 N peak pivot reaction and a 34.3 N m peak long-arm root moment; these feed the shaft, stress and deflection checks.
The SolidWorks package includes the full assembly, exploded views, component drawings and a 26-item bill of materials. It preserves adjustment at the release and counterweight interfaces.

We tested the manufactured mechanism with tennis-ball projectiles. Friction, flexibility and release behaviour exposed the limits of the clean numerical model and provided a basis for calibration.
