CREX-B French Unmanned Aerial Vehicle (UAV)
CREX-B
Tactical Unmanned Aerial Vehicle (UAV)
Other
Basic Information
Name
CREX-B French Unmanned Aerial Vehicle (UAV)
Designation
CREX-B
Alternate Designation
CREX-B
Equipment Type
Tactical Unmanned Aerial Vehicle (UAV)
Manufacturer
Leonardo
Date of Introduction
2022
Description
The CREX-B French Unmanned Aerial Vehicle (UAV) is a micro-unmanned aerial vehicle (Micro-UAV) designed for intelligence, surveillance, target acquisition, and reconnaissance (ISTAR) missions. The CREX-B provides "organic" intelligence capabilities to small units. Instead of requesting support from higher command (which takes time), a squad leader can deploy the CREX-B to see behind a building or over a ridge immediately. Its electric motor makes it nearly silent at operational altitudes, preventing detection by the enemy.
Air & Air Defense Specifications
Engine
Electric motor (low acoustic signature)
Max Speed
110.0 km/h
Cruise Speed
36.0 km/h
Range
10.0 km
Endurance
75.00 hrs
Service Ceiling
3100 m
Wingspan
1.70 m
System
Alternate Designation
CREX-B
Type
Unmanned Aerial Vehicle (UAV)
Manufacturer
Leonardo
Airframe
It features a modular, lightweight carbon-fiber construction designed for rapid deployment. The system can be assembled and launched by a single operator in minutes.
Payload Capacity
INA
Sensors and Payload
The CREX-B carries a stabilized micro-gimbal that provides high-fidelity imagery despite the platform's small size. EO/IR Sensor: Dual-sensor payload combining:
Electro-Optical (EO): Color daylight camera for positive identification. Infrared (IR): Uncooled thermal camera for night operations and heat signature detection (e.g., locating hidden personnel or vehicles). Targeting: Onboard video processing allows for target tracking and coordinate generation, which can be relayed to artillery or close air support units.
Launch
Hand-launched (bungee or simple throw).
Recovery
Deep-stall landing (belly landing) or parachute, allowing it to land in confined spaces without a runway.
Dimensions
Length
0.45 m
Height
INA
Wingspan
1.7 m
Maximum Takeoff Weight
2.1 kg
Automotive
Engine Name
INA
Engine Type
Electric motor (low acoustic signature)
Engine Power
INA
Maximum Speed
110km/h
Cruise Speed
36 km/h
Maximum Range
10 km
Operational Altitude
30–500 m Above Ground Level (AGL)
Service Ceiling
3,100 m
Endurance
75 minutes (at maximum take off weight at sea level).
Details
Country of Origin
France
Category
UAVs
Air > UAVs
Filter Label
C
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
0.45 m
Width
1.7 m
Height
—
Weight
2.1 kg
Operators (1)
France
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