Update UAV specifications and enhance performance metrics in the GPS-Denied system documentation. Refine acceptance criteria and clarify operational constraints for improved understanding.

2026-04-22 11:16:37 +00:00 · 2026-03-17 18:35:56 +02:00
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+# Solution Draft (Rev 02)
+
+## Revised Constraints (vs Draft 01)
+
+| Constraint | Draft 01 | Draft 02 |
+|-----------|----------|----------|
+| Cost per unit | $100k prototype | < $7k, target < $5k |
+| Material | CFRP (T700) | S2 fiberglass (radio transparent) |
+| Radio transparency | Not considered | Required — full RF transparency for GPS, telemetry, data links |
+| Flight time | 5-6 hours target | Same if possible, can be less |
+| Transport | Not specified | Disassembled fits in car trunk; 2 planes per pickup truck |
+
+## Product Solution Description
+
+A modular, radio-transparent electric fixed-wing reconnaissance UAV built with **S2 fiberglass/foam-core sandwich construction** with internal **carbon fiber spar reinforcement**. Designed for field deployment — disassembles into 3 sections (2 wing panels + fuselage) that fit in a car trunk, with 2 complete aircraft fitting in a standard pickup truck bed. Powered by semi-solid state batteries for maximum endurance.
+
+**Target performance**: 3.5-5 hours practical flight endurance, 9-10 kg MTOW, ~3m wingspan, < $5k BOM per unit.
+
+```
+┌──────────────────────────────────────────────────────────────┐
+│                  MODULAR AIRFRAME LAYOUT                      │
+│                                                              │
+│   LEFT WING PANEL        FUSELAGE         RIGHT WING PANEL   │
+│   (~1.5m span)          (~1.0-1.1m)       (~1.5m span)      │
+│  ┌──────────────┐   ┌──────────────┐   ┌──────────────┐     │
+│  │ S2 FG skin   │   │ S2 FG skin   │   │ S2 FG skin   │     │
+│  │ PVC foam core│◄─►│ Battery bay  │◄─►│ PVC foam core│     │
+│  │ CF spar cap  │   │ Payload bay  │   │ CF spar cap  │     │
+│  │ (internal)   │   │ Motor+ESC    │   │ (internal)   │     │
+│  └──────────────┘   └──────────────┘   └──────────────┘     │
+│                                                              │
+│  Wing-fuselage joint: aluminum spar joiner + 2 pin locks     │
+│  Assembly time target: < 10 minutes                          │
+│  Material: S2 fiberglass = RF transparent (GPS/telemetry OK) │
+│  Internal CF spar: minimal RF impact (narrow linear element)  │
+└──────────────────────────────────────────────────────────────┘
+
+TRANSPORT CONFIGURATION (standard pickup truck, 6.5ft bed):
+┌───────────────────────────────────────────┐
+│  Truck bed: 198cm × 130cm (wheel wells)   │
+│  ┌──────────────────┐ ┌────────────────┐  │
+│  │ Plane 1 wings    │ │ Plane 2 wings  │  │
+│  │ (2 × 150cm long) │ │ (2 × 150cm)    │  │
+│  │ stacked ~20cm    │ │ stacked ~20cm  │  │
+│  ├──────────────────┤ ├────────────────┤  │
+│  │ Plane 1 fuselage │ │ Plane 2 fuse.  │  │
+│  │ (~110cm)         │ │ (~110cm)       │  │
+│  └──────────────────┘ └────────────────┘  │
+│  Total width: ~60cm × 2 = 120cm < 130cm ✓│
+│  Total length: 150cm < 198cm ✓            │
+└───────────────────────────────────────────┘
+```
+
+## Existing/Competitor Solutions Analysis
+
+| Platform | MTOW | Endurance | Payload | Material | RF Transparent | Modular | Price |
+|----------|------|-----------|---------|----------|---------------|---------|-------|
+| Albatross (kit) | 10 kg | 4 hours | 4.5 kg | Fiberglass + CF | Partial | No (removable wings) | $1,500 kit |
+| Albatross (RTF) | 10 kg | 4 hours | 4.5 kg | Fiberglass + CF | Partial | No | $4,800 |
+| DeltaQuad Evo | 10 kg | 4.5h / 8.9h record | 1-3 kg | FG + CF + Kevlar | Partial | Wing removable | $25,000+ |
+| Skywalker X8 | ~4 kg | 45-60 min | 1-2 kg | EPO foam | Yes | No | $489-598 |
+| Mugin 2600 | 15 kg | 1.5-5h | 4 kg | Carbon fiber | No | Wing sections | $2,299+ |
+
+**Key insight**: The Albatross kit at $1,500 proves that a 3m wingspan composite airframe is achievable at very low cost. Our target of < $5k per complete unit (with batteries) is realistic. No competitor offers the combination of radio transparency + modular transport + semi-solid batteries.
+
+## Architecture
+
+### Component: Frame Material
+
+| Solution | Advantages | Limitations | Cost (per unit) | Fit |
+|----------|-----------|-------------|----------------|-----|
+| **S2 fiberglass skin + PVC foam core + internal CF spar (recommended)** | RF transparent skin, strong internal structure, good impact tolerance, easy to repair, $8-19/m² fabric | ~30-40% heavier than pure CFRP for equivalent stiffness | Fabric: $200-400; foam: $100-200; CF spar material: $50-100; resin: $80-150; total materials: $430-850 | ✅ Best balance of RF transparency, cost, repairability |
+| E-glass fiberglass (instead of S2) | Cheapest glass option (~$3-5/m²), RF transparent, easy to work | 40% weaker than S2, requires thicker layup → heavier | Materials: $200-500 | ⚠️ Acceptable budget option, slightly heavier |
+| Pure S2 fiberglass (no CF spar) | Maximum RF transparency, simplest construction | Insufficient wing stiffness at low weight, flutter risk | Materials: $300-600 | ❌ Stiffness deficit at acceptable weight |
+| Pure CFRP (draft 01 approach) | Lightest, stiffest | Blocks RF — GPS/telemetry degraded, expensive | Materials: $800-1500 | ❌ Fails radio transparency requirement |
+
+**Recommendation**: S2 fiberglass skin over PVC foam core with unidirectional carbon fiber spar caps (top and bottom of main spar, internal). The CF spar is a narrow linear element (~20-30mm wide per cap) inside the wing — negligible RF blockage. All external surfaces are S2 FG = fully radio transparent.
+
+### Component: Construction Method
+
+| Solution | Advantages | Limitations | Cost | Fit |
+|----------|-----------|-------------|------|-----|
+| **Vacuum-bagged foam sandwich (recommended)** | Good quality (53% stronger than hand layup), low tooling cost, reproducible | Requires vacuum pump + consumables | Equipment: $500 one-time; consumables: $50-100/unit | ✅ Best for low-cost production |
+| Hand layup over foam core | Cheapest, simplest, no equipment needed | Lower quality (more voids), less consistent | Minimal equipment | ⚠️ Acceptable for prototypes only |
+| Vacuum infusion | Best quality (71% stronger than hand layup) | More complex setup, higher consumable cost | Equipment: $1000+; consumables: $100-200/unit | ⚠️ Worth it at higher volume (>20 units) |
+| Outsourced prepreg manufacturing | Highest quality | Expensive per unit at low volume | $2000-5000/airframe | ❌ Exceeds per-unit budget |
+
+### Component: Foam Core
+
+| Solution | Advantages | Limitations | Cost/m² | Fit |
+|----------|-----------|-------------|---------|-----|
+| **PVC Divinycell H60 (recommended)** | Good stiffness/weight, closed-cell, 80°C tolerant, industry standard | More expensive than XPS | $50-80/m² | ✅ Best value for production |
+| XPS (extruded polystyrene) | Cheapest closed-cell, easy to shape with hot wire | Lower compressive strength, 75°C limit | $10-20/m² | ✅ Good budget alternative |
+| EPS (expanded polystyrene) | Very cheap | Absorbs moisture, lowest strength | $5-10/m² | ⚠️ Only for non-critical areas |
+
+### Component: Wing-Fuselage Joint (Modular Assembly)
+
+| Solution | Advantages | Limitations | Cost | Fit |
+|----------|-----------|-------------|------|-----|
+| **Aluminum spar joiner + pin locks (recommended)** | Quick assembly (<5 min), proven in RC/UAV, high strength, replaceable | Adds ~100-150g per joint (200-300g total) | $30-60 machined aluminum parts | ✅ Simple, reliable, fast |
+| 3D-printed spar connector with hinge | Very fast assembly (<2 min), lightweight | Lower strength, fatigue concerns, requires testing | $10-20 per set | ⚠️ Good for prototype, risky for production |
+| Bolted flange joint | Very strong, proven in full-scale aviation | Heavier (~200g per joint), slower assembly (10+ min) | $20-40 | ⚠️ Over-engineered for this scale |
+
+**Design**: Wing spar is a carbon fiber tube or C-channel running the full wing half-span. At the root, it slides into an aluminum joiner tube embedded in the fuselage. Secured with 2 quick-release pins (top and bottom). Electrical connections (servo leads) via a quick-disconnect plug at each wing root.
+
+### Component: Battery Technology
+
+| Solution | Energy density | Endurance impact | Cycle life | Cost/pack | Fit |
+|----------|---------------|-----------------|------------|-----------|-----|
+| **Semi-solid Tattu 330Wh/kg 6S (recommended)** | 315 Wh/kg pack | Baseline (best) | 800-1200 | ~$800-1200 est. | ✅ Best endurance per $ |
+| Semi-solid Grepow 300Wh/kg 6S | 280-300 Wh/kg pack | -5 to -10% | 1200+ | ~$700-1000 est. | ✅ Good alternative |
+| Li-Ion 21700 custom pack (6S) | 200-220 Wh/kg pack | -25 to -35% | 500-800 | ~$200-400 | ⚠️ Budget option, significant endurance loss |
+| LiPo 6S (standard RC) | 150-180 Wh/kg pack | -40 to -50% | 200-500 | ~$100-200 | ❌ Too much endurance loss |
+
+## Weight Budget (S2 Fiberglass Build)
+
+| Component | Weight (kg) | Notes |
+|-----------|-------------|-------|
+| Bare airframe (S2 FG sandwich + CF spar) | 3.8-4.5 | ~30% heavier than pure CFRP; Albatross FG+CF is 3.35 kg |
+| Wing joints (aluminum) | 0.2-0.3 | Spar joiners + pins + quick-disconnect plugs |
+| Motor + ESC + propeller | 0.4-0.6 | |
+| Wiring, connectors, misc | 0.3-0.4 | |
+| **Platform subtotal** | **4.7-5.8** | |
+| Payload (camera + gimbal + Jetson + Pixhawk + GPS) | 1.47 | Fixed |
+| Battery (semi-solid) | 2.7-3.8 | Remainder to MTOW |
+| **Total (target MTOW 10 kg)** | **~10.0** | |
+
+Conservative estimate: platform 5.3 kg + payload 1.47 kg + battery 3.2 kg = 9.97 kg.
+
+## Endurance Estimate (S2 Fiberglass)
+
+**Assumptions**:
+- MTOW: 10 kg
+- Platform weight: 5.3 kg (S2 FG airframe + motor + wiring + joints)
+- Payload: 1.47 kg
+- Battery: 3.23 kg semi-solid at 310 Wh/kg = 1001 Wh
+- Cruise power: ~140W (slightly higher than CFRP due to heavier aircraft → higher induced drag)
+- Payload power: ~30W (Jetson + camera + gimbal)
+- Total system power: ~170W
+- Battery reserve: 20%
+- Usable energy: 1001 × 0.80 = 801 Wh
+- Real-world efficiency factor: 0.75
+
+**Theoretical endurance**: 1001 / 170 = 5.9 hours
+**Practical endurance (with reserve)**: 801 / 170 ≈ **4.7 hours**
+**Practical endurance (with reserve + real-world losses)**: 801 × 0.75 / 170 ≈ **3.5 hours**
+
+**Comparison to Draft 01 (CFRP)**:
+- Draft 01: 5.0 hours practical → Draft 02: 3.5-4.7 hours practical
+- Endurance reduction: ~15-30% depending on conditions
+- Still competitive with Albatross (4h with LiPo) when using semi-solid batteries
+
+**With budget Li-Ion pack instead** (to stay under $5k):
+- 3.23 kg Li-Ion at 210 Wh/kg = 678 Wh → usable 542 Wh
+- Practical: 542 / 170 ≈ **3.2 hours** (reserve only) / **2.4 hours** (worst case)
+
+## BOM Cost Estimate (Per Unit)
+
+| Component | Low Est. | High Est. | Notes |
+|-----------|----------|-----------|-------|
+| S2 fiberglass fabric | $150 | $300 | ~8-10 m² at $15-30/m² |
+| PVC foam core (Divinycell H60) | $100 | $200 | Wing + fuselage panels |
+| Epoxy resin + hardener | $80 | $150 | ~2-3 kg resin |
+| CF spar material (tube + UD tape) | $50 | $100 | Spar caps + tubes |
+| Aluminum spar joiners (machined) | $30 | $60 | 2 joiner sets, batch machined |
+| Vacuum bagging consumables | $30 | $60 | Bag, breather, peel ply, tape |
+| Motor (brushless, ~500W) | $80 | $150 | |
+| ESC (40-60A) | $40 | $80 | |
+| Propeller (folding) | $15 | $30 | |
+| Servos (4× ailerons + elevator + rudder) | $60 | $120 | |
+| Wiring, connectors, hardware | $50 | $100 | |
+| Semi-solid battery (Tattu 330Wh/kg 6S 33Ah) | $800 | $1,200 | Single pack |
+| RC receiver | $30 | $80 | |
+| Telemetry radio | $100 | $300 | |
+| Transport case / padded bag | $50 | $150 | |
+| **Subtotal (airframe + propulsion + battery)** | **$1,665** | **$3,080** | |
+| Pixhawk 6x + GPS | $300 | $500 | If not already owned |
+| **Total BOM (without mission payload)** | **$1,965** | **$3,580** | |
+| **Total BOM (with Pixhawk, without mission payload)** | **$2,265** | **$4,080** | |
+
+Manufacturing labor (per unit, assuming in-house build with molds amortized):
+- First unit (mold making): +$2,000-3,000 tooling
+- Subsequent units: ~$500-1,000 labor per airframe (8-16 hours assembly)
+
+**Per-unit cost at batch of 5+**: **$2,800-4,500** (without mission payload) ✅ Under $5k target
+**Per-unit cost at batch of 1 (first prototype)**: **$5,000-7,000** (includes tooling) ✅ Under $7k target
+
+## Modular Transport Specifications
+
+| Dimension | Value |
+|-----------|-------|
+| Wing panel length | ~1.50 m (half-span) |
+| Wing panel chord | ~0.25-0.30 m |
+| Wing panel thickness | ~0.04-0.05 m |
+| Fuselage length | ~1.00-1.10 m |
+| Fuselage width/height | ~0.15-0.20 m |
+| Assembly time | < 10 minutes (target) |
+| Disassembly time | < 5 minutes |
+
+**Car trunk fit**: 3 sections (2 wings + fuselage) fit in standard sedan trunk (~120×80×45 cm). Wings stack flat, fuselage alongside. ✅
+
+**Pickup truck (2 planes)**: Standard 6.5ft bed (198×130 cm between wheel wells). Each plane's longest component is 150 cm (< 198 cm bed length). Two planes side by side need ~120 cm width (< 130 cm between wheel wells). ✅
+
+## Trade-off Summary: S2 Fiberglass vs CFRP
+
+| Dimension | S2 Fiberglass (Draft 02) | CFRP (Draft 01) | Winner |
+|-----------|--------------------------|-----------------|--------|
+| RF transparency | ✅ Excellent — transparent to GPS, telemetry, data links | ❌ Blocks RF, requires external antennas | S2 FG |
+| Cost per unit | $2,800-4,500 | $30,000-60,000 (prototype) | S2 FG |
+| Endurance | 3.5-4.7 hours practical | 5.0 hours practical | CFRP (+15-30%) |
+| Airframe weight | 3.8-4.5 kg bare | 2.8-3.2 kg bare | CFRP (-25%) |
+| Impact resistance | Good (fiberglass is tough) | Poor (CFRP is brittle) | S2 FG |
+| Field repairability | Easy (fiberglass patches, epoxy) | Difficult (specialized repair) | S2 FG |
+| Manufacturing complexity | Low (basic vacuum bagging) | Medium-High (precise layup) | S2 FG |
+| Transport / modularity | Same | Same | Tie |
+
+**Conclusion**: S2 fiberglass is the clear choice given the revised constraints. The 15-30% endurance reduction vs CFRP is offset by radio transparency (critical for the mission), 10x lower cost, and significantly easier manufacturing and field repair.
+
+## Testing Strategy
+
+### Integration / Functional Tests
+- Static wing load test: 3× max flight load at spar joiner (verify no failure at 3g)
+- Wing joint cycling: 100× assembly/disassembly, verify no wear or looseness
+- RF transparency test: measure GPS signal strength through airframe skin vs free-air (target: < 3 dB attenuation)
+- Assembly time test: verify < 10 minutes from transport case to flight-ready
+- Range/endurance test: fly at cruise until 20% reserve, measure actual vs predicted
+- Payload integration test: all electronics function under vibration
+
+### Non-Functional Tests
+- Transport test: load 2 planes in pickup truck, drive 100 km on mixed roads, verify no damage
+- Hard landing test: belly landing at 2 m/s descent, verify structural integrity
+- Field repair test: simulate wing skin puncture, repair with FG patch + epoxy, verify airworthy in < 30 minutes
+- Temperature test: battery + avionics function at -10°C and +45°C
+- Battery cycle test: 50 charge/discharge cycles, verify ≥95% capacity retention
+
+## Production BOM: 5 UAVs From Scratch
+
+### A. One-Time Equipment & Tooling
+
+| Item | Qty | Unit Price | Total | Notes |
+|------|-----|-----------|-------|-------|
+| **Composite Workshop Equipment** | | | | |
+| Vacuum pump (6 CFM 2-stage) | 1 | $280 | $280 | VIOT or equivalent |
+| Vacuum bagging starter kit (gauges, tubing, valves, connectors) | 1 | $150 | $150 | |
+| Digital scale (0.1g precision, 5 kg capacity) | 1 | $50 | $50 | For resin mixing |
+| Mixing cups, squeegees, rollers, brushes set | 1 | $80 | $80 | |
+| Large work table (4×8 ft plywood + sawhorses) | 1 | $150 | $150 | |
+| Self-healing cutting mat (4×8 ft) | 1 | $80 | $80 | |
+| **Foam Cutting** | | | | |
+| CNC hot wire foam cutter (4-axis, DIY kit) | 1 | $350 | $350 | Vortex-RC or similar |
+| **Mold Making** | | | | |
+| MDF sheets for plugs (4×8 ft × ¾") | 4 | $45 | $180 | Wing + fuselage plugs |
+| Tooling epoxy + fiberglass for female molds | 1 | $600 | $600 | 2× wing mold halves + fuselage molds |
+| Mold release agent (PVA + wax) | 1 | $60 | $60 | |
+| Filler / fairing compound | 1 | $80 | $80 | For plug finishing |
+| Sandpaper assortment (80-600 grit) | 1 | $40 | $40 | |
+| **Metal Work** | | | | |
+| Aluminum spar joiner machining (batch of 12 sets) | 1 | $400 | $400 | CNC outsourced, 10 sets + 2 spare |
+| **PPE & Ventilation** | | | | |
+| Respirator (half-face, organic vapor + P100) | 2 | $40 | $80 | 1 per worker |
+| Nitrile gloves (box of 200) | 2 | $25 | $50 | |
+| Safety glasses | 3 | $10 | $30 | |
+| Portable fume extractor / fan | 1 | $120 | $120 | |
+| **Hand & Power Tools** | | | | |
+| Drill + mixing paddle | 1 | $80 | $80 | |
+| Jigsaw | 1 | $60 | $60 | |
+| Rotary tool (Dremel) | 1 | $50 | $50 | |
+| Heat gun | 1 | $35 | $35 | |
+| Scissors, utility knives, rulers, clamps | 1 | $80 | $80 | Assorted set |
+| **Charging & Testing** | | | | |
+| Battery charger (6S/12S balance, 1000W) | 1 | $200 | $200 | |
+| Multimeter | 1 | $30 | $30 | |
+| Servo tester | 1 | $15 | $15 | |
+| **Software & Design** | | | | |
+| CAD/CAM (FreeCAD / OpenVSP — free) | — | $0 | $0 | Open source |
+| Hot wire CNC software (included with cutter) | — | $0 | $0 | |
+| | | | | |
+| **EQUIPMENT & TOOLING TOTAL** | | | **$3,335** | |
+
+### B. Raw Materials (for 5 UAVs + 20% waste margin)
+
+Material quantities per UAV:
+- Wing skin area: ~1.6 m² planform × 2 (top+bottom) × 2 layers = ~6.4 m² S2 fabric
+- Fuselage skin: ~0.6 m² × 2 layers = ~1.2 m²
+- Tail surfaces: ~0.3 m² × 2 layers = ~0.6 m²
+- Total S2 fabric per UAV: ~8.2 m² → with waste: ~10 m²
+- Foam core per UAV: ~2.5 m² (wings + tail)
+- Resin per UAV: ~2.5 kg (fabric weight × 1:1 ratio + extra)
+
+| Item | Qty (5 UAVs + margin) | Unit Price | Total | Notes |
+|------|----------------------|-----------|-------|-------|
+| **Structural Materials** | | | | |
+| S2 fiberglass fabric 6oz (30" wide) | 70 yards (~64 m) | $12.50/yard | $875 | ~10 m² per UAV × 5 + waste |
+| PVC foam Divinycell H60 10mm (1.22×0.81m sheets) | 16 sheets | $40/sheet | $640 | ~2.5 m² per UAV × 5 + waste |
+| Laminating epoxy resin (West System 105 or equiv) | 4 gallons | $125/gal | $500 | ~2.5 kg resin per UAV |
+| Epoxy hardener | 2 gallons | $80/gal | $160 | |
+| Carbon fiber tube (spar, 20mm OD, 1.5m) | 12 | $25 each | $300 | 2 per UAV + spare |
+| Carbon fiber UD tape (spar caps, 25mm wide) | 30 m | $5/m | $150 | 5m per UAV + spare |
+| **Vacuum Bagging Consumables** | | | | |
+| Vacuum bag film (5m × 1.5m rolls) | 6 rolls | $20/roll | $120 | ~1 roll per UAV + spare |
+| Peel ply fabric | 20 yards | $5/yard | $100 | |
+| Breather cloth | 20 yards | $4/yard | $80 | |
+| Sealant tape | 6 rolls | $12/roll | $72 | |
+| **Hardware (per 5 UAVs)** | | | | |
+| Aluminum spar joiners | (included in tooling) | — | $0 | Batch machined above |
+| Quick-release pins (stainless) | 20 | $3 each | $60 | 4 per UAV |
+| Quick-disconnect electrical plugs | 10 | $8 each | $80 | 2 per UAV (wing roots) |
+| Misc hardware (bolts, nuts, hinges, control horns) | 5 sets | $30/set | $150 | |
+| | | | | |
+| **RAW MATERIALS TOTAL (5 UAVs)** | | | **$3,287** | |
+| **Per UAV materials** | | | **~$657** | |
+
+### C. Electronics & Propulsion (per UAV × 5)
+
+| Item | Qty/UAV | Unit Price | Per UAV | ×5 Total | Notes |
+|------|---------|-----------|---------|----------|-------|
+| Motor (brushless ~500W, e.g. Dualsky XM5050EA) | 1 | $90 | $90 | $450 | Fixed-wing optimized |
+| ESC (40-60A, BLHeli) | 1 | $50 | $50 | $250 | |
+| Folding propeller (13×8 or similar) | 2 | $15 | $30 | $150 | 1 spare per UAV |
+| Servos (digital metal gear, 15-20 kg·cm) | 5 | $25 | $125 | $625 | 2× aileron + elevator + rudder + flap/spare |
+| Pixhawk 6X Mini + GPS | 1 | $380 | $380 | $1,900 | |
+| RC receiver (long range, e.g. TBS Crossfire) | 1 | $60 | $60 | $300 | |
+| RFD900x telemetry pair (shared GCS unit) | 1 air + 0.2 GCS | $170 (air) | $170 | $850 + $350 GCS = $1,200 | 1 GCS module shared |
+| Power distribution board + BEC | 1 | $25 | $25 | $125 | |
+| Wiring, connectors (XT90, JST, servo ext.) | 1 set | $40 | $40 | $200 | |
+| Semi-solid battery (Tattu 330Wh/kg 6S 33Ah) | 1 | $732 | $732 | $3,660 | |
+| | | | | | |
+| **ELECTRONICS TOTAL (5 UAVs)** | | | | **$8,910** | |
+| **Per UAV electronics** | | | **~$1,702** | | Excl. shared GCS telemetry |
+
+### D. Consumables & Misc (for 5 UAVs)
+
+| Item | Total | Notes |
+|------|-------|-------|
+| Transport bags / padded cases (per UAV) | $300 | $60 × 5 (padded wing bags + fuselage bag) |
+| Battery charger cables + adapters | $50 | |
+| Field repair kit (S2 FG patches, epoxy sachets, sandpaper) | $150 | $30 × 5 |
+| Spare hardware kit (pins, bolts, servo horns) | $100 | |
+| Shipping / freight (materials + components) | $400 | Estimate |
+| **CONSUMABLES TOTAL** | **$1,000** | |
+
+### E. Labor
+
+| Role | People | Duration | Rate | Total | Notes |
+|------|--------|----------|------|-------|-------|
+| Mold making + setup (one-time) | 2 | 3 weeks | $30/hr | $7,200 | 2 people × 40h/wk × 3 wk |
+| Airframe layup + cure (per UAV) | 2 | 3 days | $30/hr | $2,880 | 2 people × 8h × 3 days × 5 UAVs |
+| Post-cure trim, finish, assembly | 1 | 2 days | $30/hr | $2,400 | 1 person × 8h × 2 days × 5 |
+| Electronics integration + wiring | 1 | 1.5 days | $35/hr | $2,100 | 1 person × 8h × 1.5 days × 5 |
+| QA, testing, calibration | 1 | 1 day | $35/hr | $1,400 | 1 person × 8h × 1 day × 5 |
+| **LABOR TOTAL** | | | | **$15,980** | |
+| **Per UAV labor** | | | | **~$2,516** | Including amortized mold making |
+
+### F. Production Summary — Total Investment for 5 UAVs
+
+| Category | Total | Per UAV |
+|----------|-------|---------|
+| A. Equipment & Tooling (one-time) | $3,335 | $667 |
+| B. Raw Materials | $3,287 | $657 |
+| C. Electronics & Propulsion | $8,910 | $1,782 |
+| D. Consumables & Misc | $1,000 | $200 |
+| E. Labor | $15,980 | $3,196 |
+| | | |
+| **GRAND TOTAL (5 UAVs)** | **$32,512** | |
+| **Per UAV (all-in, including labor)** | | **$6,502** |
+| **Per UAV (materials + electronics only, no labor)** | | **$3,306** |
+
+### G. Cost Optimization Options
+
+| Optimization | Savings/UAV | Impact |
+|-------------|-------------|--------|
+| Use XPS foam instead of Divinycell H60 | -$90 | Slightly lower stiffness, acceptable for prototype |
+| Use E-glass instead of S2 glass | -$100 | ~40% weaker, needs thicker layup → ~200g heavier |
+| Use Li-Ion 21700 pack instead of Tattu semi-solid | -$400 | Endurance drops from 3.5-4.7h to 2.4-3.2h |
+| Self-machine spar joiners (manual lathe) | -$50 | Requires metalworking skill |
+| Use cheaper servos ($15 each) | -$50 | Lower torque, shorter lifespan |
+| **Aggressive budget build** | **-$690** | **$2,616/UAV materials only** |
+
+### H. Minimum Viable Team
+
+| Role | Count | Skills Required | Commitment |
+|------|-------|----------------|------------|
+| Composite fabricator | 1-2 | Fiberglass layup, vacuum bagging, mold making | Full-time during build (8 weeks) |
+| Electronics/avionics tech | 1 | Soldering, Pixhawk configuration, wiring | Part-time (can overlap with fabricator) |
+| **Minimum: 2 people for 8 weeks** | | | |
+
+**Timeline for 5 UAVs**:
+- Week 1-3: Mold making (CNC foam plugs → fiberglass female molds)
+- Week 4-5: First 2 airframes layup + cure + trim
+- Week 5-6: Next 3 airframes layup + cure + trim
+- Week 6-7: Electronics integration all 5 units
+- Week 7-8: Testing, calibration, flight testing
+- **Total: ~8 weeks with 2 people**
+
+### I. Minimal Absolute Cost (No Labor Accounted)
+
+If labor is free (owner-operators building their own):
+
+| Category | Total | Per UAV |
+|----------|-------|---------|
+| Equipment & Tooling | $3,335 | $667 |
+| Raw Materials | $3,287 | $657 |
+| Electronics & Propulsion | $8,910 | $1,782 |
+| Consumables & Misc | $1,000 | $200 |
+| **TOTAL (5 UAVs, no labor)** | **$16,532** | |
+| **Per UAV (no labor)** | | **$3,306** |
+
+**Absolute minimum per UAV** (with budget optimizations from Section G): **~$2,616**
+
+## References
+
+1-20: See Draft 01 references (all still applicable)
+
+Additional sources:
+21. S-Glass vs E-Glass comparison: https://wiki-science.blog/s-glass-vs-e-glass-key-differences
+22. Reinforcement Fiber Reference: https://explorecomposites.com/materials-library/fiber-ref/
+23. S-Glass vs Carbon Fiber: https://carbonfiberfriend.com/s-glass-vs-carbon-fiber/
+24. RF Attenuation by composite materials: https://www.rocketryforum.com/threads/rf-attenuation-by-body-tube-nosecone.186634/
+25. Russian foamplast UAV (max radio transparency): https://bulgarianmilitary.com/2023/10/15/russia-unveils-foamplast-fpv-uav-with-max-radio-transparency/
+26. Albatross UAV Kit: https://store.appliedaeronautics.com/albatross-uav-kit/
+27. UAV spar connector development: https://www.konelson.net/home/spar-connector-development
+28. Scabro Innovations UAV prototyping: https://scabroinnovations.com/diensten/composite-airframe-prototyping/
+29. Tattu 330Wh/kg 6S pricing — GenStattu: https://genstattu.com/tattu-semi-solid-state-330wh-kg-33000mah-10c-22-2v-6s1p-g-tech-lipo-battery-pack-with-xt90-s-plug/
+30. Pixhawk 6X pricing — Holybro: https://holybro.com/products/pixhawk-6x-rev3
+31. RFD900x pricing — DrUAV: https://druav.com/products/rfdesign-rfd900x
+32. Composite workshop setup — Fibre Glast: https://www.fibreglast.com/blogs/learning-center/setting-up-a-composite-shop
+33. CNC hot wire foam cutter — Vortex-RC: https://www.vortex-rc.com/product/4-axis-diy-hot-wire-cnc-for-rc-hobbyists-aeromodellers-and-designers/
+34. Composite mold making — Canuck Engineering: https://www.canuckengineering.com/capabilities/composite-molds/