




| Name | Airbus U030 Flexrotor |
| Manufacturer | Airbus Helicopters (formerly Aerovel) |
| Country of Origin | United States (production in Bingen, WA) |
| Type / Role | Group 2 small tactical VTOL UAS / ISTAR |
| First Flight / Introduced | Early 2010s (Aerovel); Airbus portfolio 2024 |
| Status | In service / production |
| Unit Cost | Not publicly disclosed |
| Maximum Speed | 140 km/h (77 kt dash) |
| Cruise Speed | ~78โ87 km/h (min/typical) |
| Operational Range | Endurance-limited (line-of-sight/BLOS) |
| Endurance | 12โ15 hours typical |
| Service Ceiling | >5,000 m (16,400 ft) |
| Rate of Climb | Not publicly detailed |
| Length | 2 m (6.6 ft) |
| Wingspan | 3 m (9.8 ft) |
| Height | 2.2 m |
| Maximum Takeoff Weight (MTOW) | 25 kg (55 lb) |
| Payload Capacity | 8 kg (18 lb) |
| Hardpoints | Modular payload bay (no fixed hardpoints listed) |
| Weapons | None (ISR-focused) |
| Sensors | EO/IR, radar, and other advanced modular sensors |
| Avionics | Autonomous flight control, GPS/INS, real-time data link |
| Engine Type | 28 cc two-stroke |
| Engine Power | Not publicly detailed |
| Propeller Type | Rotor for VTOL + wing-borne cruise |
| Control Type | Fully autonomous / remote |
| Data Link Range | Line-of-sight (extended BLOS options, e.g., Starlink in some configs) |
| Navigation | GPS / INS (GPS-denied capable) |
| Ground Control Station | Portable / expeditionary |
| Primary Users | U.S. Navy exercises, EMSA, Canada (Voyageur), Australia (Drone Forge), Uzbekistan, commercial operators |
| Combat Proven | Mission-proven in exercises and real-world surveillance |
| Notable Operations | USS Paul Hamilton launches, Baltic Sea EMSA surveillance (2026), wildfire monitoring, maritime interdiction support |
The Airbus U030 Flexrotor is a compact Group 2 tactical vertical take-off and landing (VTOL) uncrewed aircraft system optimized for persistent intelligence, surveillance, target acquisition, and reconnaissance (ISTAR) in demanding environments.
Originally developed by U.S. firm Aerovel Corporation in Bingen, Washington, and acquired by Airbus Helicopters in 2024, the Flexrotor combines rotorcraft vertical launch and recovery with efficient wing-borne cruise. It requires only a 3.7 m × 3.7 m (12 ft × 12 ft) area for autonomous operations from land or ship decks without dedicated flight decks, transitioning from stowed configuration to airborne in approximately 30 minutes.
With a maximum take-off weight of 25 kg (55 lb) and payload capacity of up to 8 kg (18 lb), the system supports modular electro-optical/infrared (EO/IR) sensors, radar, and other mission-specific payloads. Typical endurance reaches 12–15 hours, enabling persistent coverage for maritime surveillance, border security, search and rescue, firefighting support, and electronic warfare or communications relay tasks. Dash speed is listed at 140 km/h (77 kt), with minimum cruise around 78 km/h (42 kt) and service ceiling exceeding 5,000 m (16,400 ft). Propulsion comes from a 28 cc two-stroke engine capable of gasoline or heavy fuel.
The platform has demonstrated operations in harsh, high-threat, and GPS-denied conditions, including U.S. Navy exercises (such as launches from USS Paul Hamilton), European Maritime Safety Agency Baltic Sea surveillance missions starting in 2026, and commercial applications like wildfire monitoring. It supports crewed-uncrewed teaming and real-time data streaming. Unit cost is not publicly disclosed.
Designed for minimal logistical footprint, the U030 Flexrotor fills a niche for expeditionary forces needing reliable, long-endurance ISR without large support infrastructure.
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