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
- Structures: safe joining methods, reinforcement without sharp/hard hazards.
- Command & Control: risk review, pre-flight inspection checklist.
- Payload: optional “dummy payload” spec (mass + placement).
- Recovery: keep landing zone safe; plan for larger footprint.
Constraints
- Water rockets only.
- No metal pressure vessels, no glass, no dangerous projectiles.
- Only one pressurised bottle (the main pressure chamber). The second bottle is structural/aerodynamic.
- All joins must be smooth (no sharp edges); tape and lightweight materials only.
- Teacher-controlled pressurisation and release; staff-approved pressure limits.
What you must produce (deliverables)
- 1 double-bottle rocket design + build sheet.
- A pre-flight inspection checklist specific to your design (joints, symmetry, fin security).
- Launch log for 3 launches + one improvement you made based on the data.
- Short “trade-off note”: what you gained and what you risked by adding complexity.
Scaffolding Example (optional)
You are allowed to reuse structures and formats from other teams — but not their decisions.
Example architecture options (choose one)
- Inline extension: second bottle adds length (better stability) while the main bottle is the pressure chamber.
- Fairing body: second bottle shapes airflow and protects interfaces (still one pressure chamber).
- Stability sleeve: second bottle acts as a straight “spine” to keep fins and nose aligned.
Example: Interface checklist (before every launch)
- Join is smooth and fully taped (no peeling edges).
- Centre-lines match (alignment marks line up).
- Fins are identical and rigid; none flex when lightly pressed.
- Pad fit is stable; rocket doesn’t rock or twist on the latch.
Example: Evidence-led iteration (how to improve safely)
- Launch v1 → write down the single biggest problem you observed.
- Make one change only (e.g., strengthen the join OR re-angle fins).
- Launch v2 under the same conditions → compare logs.
Build & test steps
- Decide your architecture: inline extension, fairing, or stability body.
- Plan the join: alignment is everything. Mark centre-lines before taping.
- Build fins bigger/stronger than LS2 (more mass needs more stability).
- Dry-fit on the pad: ensure the pressurised bottle interfaces correctly.
- Static checks: symmetry, fin angle, secure joins, no sharp edges.
- Launch 1 (teacher-managed): safe pressure; note stability and any flex.
- Iterate: strengthen weak points; re-check symmetry.
- Launch 2–3: repeat and log for consistency.
Launch-day checklist
- Extra inspection time (interfaces fail first).
- Range clear + safety perimeter confirmed.
- Roles assigned + recorder ready.
- Clear call: “Hold” if anyone sees a joint peeling or fin coming loose.
- Recovery team waits for “all clear”.
Success criteria
- Rocket remains structurally intact through 3 launches.
- Flight is safe and mostly straight (no hazardous lateral launch).
- Team identifies at least one improvement made from logged evidence.
- Pre-flight checklist is used, not just written.
Evidence checklist
- Photos focusing on the joint/interface.
- Video of at least one full launch sequence.
- 3 completed launch logs + highlighted “change we made” note.
- Pre-flight checklist (completed) for at least one launch.
Safety rules
- Teacher-controlled pressurisation/release only.
- No one over the rocket; eye protection near the operations area.
- Stop if joints peel, bottle deforms, or alignment shifts on the pad.
- Use soft, lightweight materials for structure; avoid hard nose weights.
- Keep the range larger than LS2 (bigger rocket, bigger drift).
Common failure modes
- Misaligned bottles → wobble and sideways thrust at release.
- Weak join → mid-flight separation (unsafe debris risk).
- Extra mass without bigger fins → instability.
- Checklist ignored → repeating the same mistake.
Stretch goals
- Create a “build quality standard” poster for your team (symmetry, joint strength, fin alignment).
- Compare two join methods and decide which is best for safety + repeatability.
- Introduce a simple “go/no-go” review board (2 students + teacher) before launch.