Mission Goal

Build a two-bottle rocket airframe that improves stability and/or performance, while remaining safe, inspectable, and repeatable. Demonstrate at least 3 logged launches.

Why it matters

Scaling a launch vehicle means solving integration problems: stronger joints, alignment, mass distribution, and consistent build quality. Real rockets fail at interfaces — where stages, tanks, or structures meet.

Inputs from other teams

Constraints

What you must produce (deliverables)

Scaffolding Example (optional)

You are allowed to reuse structures and formats from other teams — but not their decisions.

Example architecture options (choose one)

Example: Interface checklist (before every launch)

Example: Evidence-led iteration (how to improve safely)

  1. Launch v1 → write down the single biggest problem you observed.
  2. Make one change only (e.g., strengthen the join OR re-angle fins).
  3. Launch v2 under the same conditions → compare logs.

Build & test steps

  1. Decide your architecture: inline extension, fairing, or stability body.
  2. Plan the join: alignment is everything. Mark centre-lines before taping.
  3. Build fins bigger/stronger than LS2 (more mass needs more stability).
  4. Dry-fit on the pad: ensure the pressurised bottle interfaces correctly.
  5. Static checks: symmetry, fin angle, secure joins, no sharp edges.
  6. Launch 1 (teacher-managed): safe pressure; note stability and any flex.
  7. Iterate: strengthen weak points; re-check symmetry.
  8. Launch 2–3: repeat and log for consistency.

Launch-day checklist

Success criteria

Evidence checklist

Safety rules

Common failure modes

Stretch goals