1.0
Objective
I led a four-person team (named “Team Team”) from a Tier D trainer to a Tier F rocket on a G80T-13 motor. We laid up our own fiberglass airframe, redesigned the fins for drag, and built a nose-cone cushion that brought the egg back intact.
2.0
Work performed
- 2.1Modeled the rocket in SolidWorks and simulated flights in OpenRocket, first for the Tier D trainer, then for Tier F.
- 2.2Replaced the elliptical fins with swept, curved fins to cut drag at ~500 ft/s².
- 2.3Estimated the parachute deployment shock from nose-cone mass and shock-cord stiffness, then designed a two-density foam cushion in the nose cone, away from motor heat.
3.0
Specification
| Motor | G80T-13 |
|---|---|
| Airframe | Two-layer fiberglass hand layup on a steel-pipe mandrel |
| Nose cone | 3D printed, minimum infill |
| Avionics | BMP388 altitude sensor with telemetry |
| Tools | SolidWorks · OpenRocket |
4.0
Plates
5.0
Anomaly report
Closed
- Observed
- Air bubbles in the first fiberglass layup.
- Corrective action
- Cut the tube and kept only the section with the best structural quality.
- Lesson
- Concentricity came from the steel mandrel. Quality came from being willing to throw material away.