VECTORDEFENCE DRONE
INTELLIGENCE
INDEPENDENT PERSPECTIVE
THE EVOLVING FIELD GUIDE
Editor

DEFENCE DRONES / THE LIBRARY

Compare the evidence.

Choose up to three systems. Specifications retain their source and configuration; missing information is left undisclosed.

Airbus U050 Capa-X

Modular French tactical UAV with a September 2026 order for Army and Navy evaluations and delivery planned in 2027.

Country / region
France
Programme status
Order / production commitment
Sources reviewed
20 Sept 2026
Order / production commitmentOrder / production commitment
Primary domain
Air
System type
Reconnaissance aircraft
Developer / manufacturer
Airbus Helicopters / Survey Copter
Origin / production countries
France
Other names
Capa-X; U050
Variants / configurations
CTOL / VTOL configurations; Short-wing and long-wing arrangements
Operators / programme customers
French Army and Navy — evaluation customers

Evidence & current status

Published performance is supplier-reported and configuration dependent; operational use does not independently validate every specification.

Role & capabilities

  • Reconnaissance aircraft

Specifications in context

Airframe
Modular fixed-wing UAV with CTOL and VTOL configurations

Manufacturer-published specification; maximum values are not necessarily simultaneous.

Source ↗
Launch / recovery
Conventional or vertical take-off and landing

Manufacturer-published specification; maximum values are not necessarily simultaneous.

Source ↗
Propulsion
Not established from the reviewed public sources.

Public data gap; no estimate or neighbouring variant value substituted.

Source ↗
Dimensions
Long-wing span 6 m; length 4 m

Manufacturer-published specification; maximum values are not necessarily simultaneous.

Source ↗
Mass
120 kg MTOW

Manufacturer-published specification; maximum values are not necessarily simultaneous.

Source ↗
Endurance
Seven hours demonstrated in evaluation; up to ten hours advertised

Manufacturer distinguishes evaluation result from maximum capability.

Source ↗
Range
100 km direct data-link range

Direct link, not total distance travelled.

Source ↗
Speed
150 km/h maximum in short-wing configuration

Manufacturer-published specification; maximum values are not necessarily simultaneous.

Source ↗
Altitude
3,000 m ceiling

Manufacturer-published specification; maximum values are not necessarily simultaneous.

Source ↗
Payload
Up to 20 kg

Manufacturer-published specification; maximum values are not necessarily simultaneous.

Source ↗
Sensors
Initial configuration: EO imagery and SIGINT

Describes ordered baseline, not all future options.

Source ↗
Communications / navigation
Not established from the reviewed public sources.

Public data gap; no estimate or neighbouring variant value substituted.

Source ↗