Per drone
182 ha/h at 120 m; 378 ha/h with an altitude waiver (representative 17 m/s cruise).
Payload capability & coverage ยท 2026-06-14
Coverage is recalculated from the optics: a 25 mm, F/2 wide-field LWIR survey optic on a 640×512, 17 um uncooled core, sized to detect a 3 cm smouldering char. The numbers below follow a fixed-wing survey aircraft across realistic platforms.
Detection-limited geometry
At the 120 m cap the optic gives 8.2 cm GSD over a 53 m swath and detection is easy. Flying higher coarsens the GSD until a 3 cm char stops being detectable: about 17 cm GSD (~253 m, 110 m swath) for a strong benchmark detection, or 24 cm (~358 m, 156 m swath) at the marginal advisory limit. Wider swath at altitude is what raises coverage.
Drone platforms considered
| Platform | Type | Cruise | Endurance | Max payload | Carries 2 kg? | Coverage @120 m | Coverage @waiver |
|---|---|---|---|---|---|---|---|
| WingtraOne GEN II | VTOL fixed-wing | 16 m/s | 59 min | 800 g | No | 171 ha/h | 355 ha/h |
| AgEagle eBee X | fixed-wing | 16 m/s | 90 min | 1000 g | No | 171 ha/h | 355 ha/h |
| Quantum Systems Trinity Pro | VTOL fixed-wing | 17 m/s | 90 min | 700 g | No | 182 ha/h | 378 ha/h |
| Delair UX11 | fixed-wing | 15 m/s | 80 min | 500 g | No | 160 ha/h | 333 ha/h |
| AeroVironment Puma 3 AE | fixed-wing | 18 m/s | 180 min | 1800 g | No | 193 ha/h | 400 ha/h |
| Event 38 E455 | hybrid VTOL | 19 m/s | 120 min | 3200 g | Yes | 203 ha/h | 422 ha/h |
| JOUAV CW-15 | VTOL fixed-wing | 17 m/s | 120 min | 3000 g | Yes | 182 ha/h | 378 ha/h |
| JOUAV CW-25 | hybrid VTOL | 23 m/s | 360 min | 6000 g | Yes | 246 ha/h | 511 ha/h |
The 2 kg column is the binding reality: most compact survey fixed-wings carry under 1 kg, so a full 2 kg payload forces the heavier Puma / E455 / JOUAV class — or the EmberScope build is trimmed toward a camera-only ~0.7–0.8 kg module to open the mainstream class.
Per-drone payload cost
| Line | First article | Recurring (per unit) |
|---|---|---|
| Detector core + interface (Boson+ 640 radiometric) | USD 6k–USD 12k | USD 6k–USD 12k |
| LWIR window / filter (Ge, AR-coated) | USD 1k–USD 4k | USD 1k–USD 3k |
| Mirror set + metrology (SPDT aluminium) | USD 15k–USD 45k | USD 5k–USD 12k |
| Mirror coating (protected gold/IR) | USD 2k–USD 8k | USD 1k–USD 4k |
| Internal blackening / baffling | USD 500–USD 3k | USD 500–USD 2k |
| Optical cassette + mounts | USD 5k–USD 15k | USD 2k–USD 6k |
| Housing, seals, drone adapter | USD 3k–USD 10k | USD 2k–USD 5k |
| Compute, storage, timing, power | USD 2k–USD 6k | USD 2k–USD 6k |
| Calibration + field-reference kit | USD 1k–USD 5k | USD 0–USD 1k |
| Assembly + metrology + first-article rework | USD 5k–USD 15k | USD 3k–USD 6k |
| Total payload | USD 46k–USD 128k | USD 22k–USD 57k |
Drone airframes are excluded from the AUD 100k payload budget. A 2 kg-capable fixed-wing is itself roughly USD 20–30k each — a separate, larger platform spend.
Fleet sizing against the budget
182 ha/h at 120 m; 378 ha/h with an altitude waiver (representative 17 m/s cruise).
Custom-optics payloads at USD 22k–USD 57k each buy 1–2 payloads within the budget.
~182–364 ha/h at 120 m, or ~378–755 ha/h with a waiver.
Hourly revisit fits a focused high-risk zone of a few square kilometres, not a whole region. Unit payload cost sets the fleet; altitude authorisation roughly doubles per-drone coverage.
Open the coverage sizing grid to convert these per-drone numbers into target-area, payload-count, and max-unit-cost thresholds.