AAMS-X1
Autonomous Aerial Mobility System
Quad-rotor aerial platform navigating on optical flow rather than satellite fix, with a four-bay underslung rack. It holds position and completes a route in the places GNSS does not reach — between buildings, under structure, inside plant.
One sortie, end to end
01 — LAUNCH · CORRIDOR · DROPRooftop launch, corridor transit, marked-pad drop and re-ascent. Scroll it as one continuous flight — because that is how it is flown.
Payload configuration
02 — FOUR-BAY RACKThe rack takes one, two or four pods. Every bay releases independently, so a single sortie can serve up to four separately addressed drops without returning to base.
Slung mass is the constraint that matters. Range and endurance fall with it, and the planner solves the route against what is actually fitted — not against the empty-aircraft figure.
- SLUNG MASS
- 7.0kg
- RANGE
- 25.7km
- ENDURANCE
- 36min
- DROPS PER SORTIE
- 2×
Provisional model. Linear mass penalty pending flight test.
Technical specification
04 — BY SUBSYSTEM01 Airframe & mass 4 PARAMETERS
- Rotor count / configuration
- 4, quad rotor with folding arms
- Rated payload
- 100 kg
- Maximum take-off mass
- ~300 kg
- Thrust-to-weight at MTOW
- ≥ 1.4
02 Flight performance 5 PARAMETERS
- Hover endurance at MTOW
- ≥ 15 min
- Hover throttle at MTOW
- ≈ 70 %
- Hover bus power
- 34 kW
- Usable pack energy
- 9.9 kWh
- Rotor-out (OEI) behaviour
- Controlled hover at reduced margin, safe landing
03 Navigation & sensing 1 PARAMETERS
- Primary navigation
- Optical flow + range, GNSS-independent
04 Payload rack 2 PARAMETERS
- Bays
- 4, independently released
- Release
- Electromechanical, per bay
05 Compute, links & compliance 2 PARAMETERS
- Compute
- OmegaMTL stack, real-time safety tier
- ESC telemetry bus
- CAN-FD, ≥ 100 Hz
Product requirements and design allocations from the current definition baseline — not measured field results.
Deployment
05 — WHERE IT FLIES- 01
Medical and diagnostic transfer
Sample and consumable movement between facilities on a fixed corridor, measured in minutes rather than traffic.
- 02
GNSS-denied inspection
Structure and asset survey between buildings, under decks and inside plant where satellite fix is unusable.
- 03
Multi-drop urban delivery
Four separately addressed pods released across one route without returning to base.
- 04
Disaster response
First-look survey and small-payload resupply into areas the ground network cannot reach.
Fly a corridor
Send us the two endpoints and the payload. We will come back with a sortie profile and what a first deployment looks like.
Request an AAMS-X1 pilot