Background
Seed dispersal in hazardous or inaccessible environments (e.g., post-wildfire zones, steep slopes) is difficult to achieve using conventional replantation methods. This project aimed to design an air-powered, biodegradable seed rocket to deliver seeds over long distances with minimal environmental impact.
Design
- Nose Cone (SLA, Tough 2000): parabolic profile for low drag and weight balancing.
- Seed Payload (SLS, PA12 Nylon): complex internal geometry with no supports required.
- Fins & Launching Base (FDM, ABS): self-supported geometry, integrated for stability.
Delivery Method
- Spiral screw-style payload release for passive mid-flight seed ejection.
- Optimized fin shape (clipped delta with rounded leading edge, wedge trailing edge) to maximize stability.
Cost & Time Summary
| Part | Process | Material | Print Time | Cost |
|—————–|———|————-|————|———|
| Fins & Base | FDM | ABS | 9 hr 15 m | $144.10 |
| Nose Cone | SLA | Tough 2000 | 3 hr 23 m | $17.29 |
| Payload Section | SLS | PA12 Nylon | 8 hr 30 m | $159.26 |
| Total | — | — | ~21 hr | $320.65 |
Simulation
- Simulated using open-source rocket flight software.
- Parameters: wind speed = 2 m/s, AoA = 45°, launch impulse = 10 Ns.
- Result: Achieved ~70 meters horizontal distance.