L1 Minimal Configuration¶
Decision¶
Fly the certification flight in minimal L1 configuration rather than full dual-deployment setup.
Configuration Differences¶
Full L2 Configuration (IMG_6434)¶
- Main body tube
- Electronics bay (e-bay) with altimeter
- Coupler tube between e-bay and nose cone
- Nose cone
- 18" drogue parachute (upper section)
- 48" main parachute (lower section)
- Dual deployment (altimeter-controlled)
Minimal L1 Configuration (IMG_7824)¶
- Main body tube (shortened - no e-bay section)
- Nose cone attached directly to body tube
- 48" main parachute only
- Motor ejection charge deployment (no electronics)
Removed Components¶
| Component | Weight Estimate | Reason |
|---|---|---|
| Electronics bay tube | ~100g | Not needed for motor ejection |
| E-bay bulkheads, sled, hardware | ~150g | No altimeter deployment |
| 18" drogue parachute | ~30g | Single deployment only |
| Coupler tube (e-bay to nose) | ~80g | Shorter rocket |
| Altimeter | ~50g | Motor ejection is sufficient |
Total removed: ~400g estimated
Rationale¶
Simplicity¶
L1 certification demonstrates basic HPR competency. Adding dual-deployment electronics introduces failure modes:
- Altimeter malfunction
- Wiring issues
- Battery problems
- Charge firing timing
- Multiple separation events
For certification, minimize variables.
Reliability¶
Motor ejection is proven technology:
- No electronics to fail
- No batteries to die
- No wiring to disconnect
- Single separation event
Regulatory¶
No pyrotechnic electronics to explain to Swedish authorities. Simpler = less questions.
Reversibility¶
After L1 certification:
- Re-install electronics bay
- Add drogue parachute
- Full dual-deployment for L2
All removed components are stored safely.
Weight Impact¶
| Configuration | Approximate Mass |
|---|---|
| Full L2 config (empty) | ~1.9 kg |
| L1 minimal (empty) | ~1.46 kg |
| L1 with motor (H128W) | ~1.67 kg |
The lighter rocket with H128W will fly higher than needed for a conservative certification flight. See L1 Weight Budget for ballast calculations.
Photos¶
| Configuration | Photo |
|---|---|
| Full L2 (painted) | |
| L1 minimal (window view) |
References¶
- Stability Calculations - CG/CP for L1 config
- L1 Weight Budget - Mass budget and ballast
- Motor Selection - H128W specifications