Space frame
I designed the frame for low weight, driver ergonomics and node-to-node triangulation, with every load-carrying mount placed on a node. I chose AISI 4130 over AISI 1010, 1018, 1020 and 1080 for its strength-to-weight ratio and weldability.
- Sketched the suspension hardpoints from the wheelbase and track width to place the first members.
- Built around the cockpit and legroom templates and the 95th-percentile driver helmet clearance (rules T3–T4).
- Laid out the main hoop, front hoop and bulkhead planes, then sized the powertrain bay and closing plane.
- Triangulated and braced the frame to the rules, then ran five static load cases in SolidWorks Simulation.
- Generated DXF files for laser cutting and designed jigs for tube notching and frame alignment during welding.
100 km/h to rest in 0.5 s gives 55.56 m/s², or 5.66 g. On a 320 kg loaded mass that is 320 × 9.81 × 5.66 = 17,767.87 N, applied over 4 nodes. Torsion cases use a 2 g couple: 320 × 9.81 × 2 = 6,278.4 N.
| Load case | Total load | Per node (×4) | Min FOS |
|---|---|---|---|
| Front impact | 17,767.87 N | 4,441.96 N | 1.4 |
| Side impact | 17,779.20 N | 4,444.80 N | 2.1 |
| Rear impact | 17,767.87 N | 4,441.96 N | 2.6 |
| Front torsion | 6,278.40 N | 1,569.60 N | 4.0 |
| Rear torsion | 6,278.40 N | 1,569.60 N | 5.3 |