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Capa-X French Unmanned Aerial Vehicle (UAV)

Capa-X

Tactical Unmanned Aerial Vehicle (UAV)
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Basic Information
Name
Capa-X French Unmanned Aerial Vehicle (UAV)
Designation
Capa-X
Alternate Designation
Capa-X
Equipment Type
Tactical Unmanned Aerial Vehicle (UAV)
Manufacturer
developed by Survey Copter, a subsidiary of Airbus Helicopters
Date of Introduction
2025
Description

The Capa-X French Unmanned Aerial Vehicle (UAV) is a light tactical Unmanned Aerial System (UAS) in the 100–150 kg class. It features a modular architecture that enables operators to reconfigure the airframe for specific mission requirements. Developed by Survey Copter, a subsidiary of Airbus, the Capa-X addresses the capability gap between smaller mini-UAVs, such as the Aliaca, and larger tactical rotary-wing drones, such as the VSR700. As of October 2025, the Capa-X is fully integrated into the Airbus Helicopters tactical UAS portfolio. It is notable for its capability to switch between Vertical Take-Off and Landing (VTOL) and Horizontal Take-Off and Landing (HTOL) configurations, as well as between short and long wingspans. This flexibility allows optimization for endurance, speed, or payload, depending on mission requirements. Intelligence, Surveillance, and Reconnaissance (ISR): The Capa-X is equipped with high-definition Electro-Optical/Infra-Red (EO/IR) gimbals, providing persistent surveillance capabilities for border control, maritime patrol, and target acquisition. ​ Manned-Unmanned Teaming (MUM-T): Under Airbus Helicopters' management, the Capa-X is integrated into the HTeaming solution. This integration enables helicopter crews to control the UAV from the cockpit and use it as a forward sensor to identify threats before manned aircraft enter the engagement zone. ​ Logistics and Cargo: The internal bay and under-fuselage hardpoints can carry up to 20 kg of cargo, facilitating the resupply of critical munitions or medical equipment to forward units. ​ Electronic Warfare and Relay: The modular bay supports the integration of Signals Intelligence (SIGINT) packages or communication relays to extend tactical networks in complex terrain.

Air & Air Defense Specifications
Engine The Capa-X utilizes a specific hybrid configuration where a 4-stroke thermal engine drives a pusher propeller for horizontal cruise flight, providing range and fuel efficiency superior to purely electric systems. For VTOL operations, it utilizes detachable booms equipped with electric lift rotors and dedicated batteries. This setup allows the thermal engine to be optimized for cruise efficiency while the electric motors handle the high-power vertical phases.
Max Speed 150.0 km/h
Range 100.0 km
Endurance 10.00 hrs
Service Ceiling 3000 m
Wingspan 6.00 m
Payload Capacity 0 kg
System
Alternate Designation Capa-X
Type Unmanned Aerial Vehicle (UAV)
Manufacturer developed by Survey Copter, a subsidiary of Airbus Helicopters.
Payload Capacity 0 kg to 20 kg; Modular bay supports multiple sensor types
Multi-Sensor Integration The fuselage features a versatile payload bay capable of "bi-payload" or "tri-payload" configurations. For example, it can simultaneously carry a nose-mounted EO/IR turret and a belly-mounted radar or cargo pod, allowing a single sortie to perform multiple distinct functions (e.g., detect with radar, identify with EO/IR, and designate).
Propulsion Modules The system can be configured as VTOL (Vertical Take-Off and Landing) for operations from confined spaces (e.g., ship decks, forest clearings) or HTOL (Horizontal Take-Off and Landing) for runway operations where maximum payload or endurance is prioritized.
Wing Modules Long Wings (6m span): Optimize the platform for high-aspect-ratio flight, extending loiter time (>10 hours) for ISR missions. ​Short Wings: Increase cruising speed (up to 150 km/h) and maneuverability for dynamic targeting or cargo delivery in contested environments.
Dimensions
Length 4.0 m
Height INA
Wingspan 6.0 m
Maximum Takeoff Weight 120 kg
Automotive
Engine Name INA
Engine Type The Capa-X utilizes a specific hybrid configuration where a 4-stroke thermal engine drives a pusher propeller for horizontal cruise flight, providing range and fuel efficiency superior to purely electric systems. For VTOL operations, it utilizes detachable booms equipped with electric lift rotors and dedicated batteries. This setup allows the thermal engine to be optimized for cruise efficiency while the electric motors handle the high-power vertical phases.
Engine Power INA
Maximum Speed 150 km/h
Cruise Speed INA
Maximum Range 100 km
Service Ceiling 3,000 m
Endurance 10 hours
Details
Country of Origin France
Category UAVs
Air > UAVs
Filter Label
C
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
4 m
Width
6 m
Height
Weight
120 kg
Operators (1)
France
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