Build Phases

The Cycle

01

Design & Simulate

We model the rocket in parametric CAD — adjusting nose cone profile, fin geometry, and body diameter until the simulation looks right. OpenRocket is our primary tool for predicting altitude, stability margin, and flight time. We iterate digitally until the numbers hit the ARC window before printing a single gram.

OpenRocket Parametric CAD Stability Analysis
02

Slice & Print

Components are sliced with careful attention to wall count, infill pattern, and layer orientation relative to load paths. The body tube, fins, nose cone, and motor mount are all printed in-house on FDM printers. We weigh every print against our mass budget and re-slice if needed.

FDM Printing PETG / PLA Mass Budget
03

Assemble & Bond

Components are assembled using structural epoxy — fins are through-the-wall mounted into slots printed directly into the body tube. We verify CG and CP location physically with a balance point check, and compare against the simulated values before any motor is loaded.

Structural Epoxy CG/CP Verification TTW Fins
04

Ground Test

Before flight day, we run through a full pre-launch checklist: parachute packing and ejection charge sizing, motor retention confirmation, and a final mass measurement. Everything is documented so we can trace any anomaly back to a specific build decision.

Pre-Launch Checklist Ejection Sizing Motor Retention
05

Launch & Debrief

On launch day, we follow range safety procedures and record every flight with a timer and altitude tracker when available. After recovery, the team debriefs: what matched the simulation, what didn't, and what changes go into the next iteration. Every flight is data.

Flight Data Debrief Iteration

Our Toolkit

Tools We Use

OpenRocket

Primary simulation environment. Used for altitude prediction, stability margin analysis, and ejection delay calculation.

CAD Software

Parametric modeling for all printed components. Geometry changes propagate instantly across the full assembly.

FDM Slicer

Controls infill density, wall count, and layer height — the levers that determine part strength and mass.

FDM Printer

All airframe components are printed in-house, giving us complete control over geometry and material choice.

Structural Epoxy

Used for all permanent bonds — fins to body tube, motor mount to airframe, and nose cone retention.

Digital Scale

Every component is weighed against the mass budget. If a print is over, we re-slice or redesign before moving on.