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Barracuda European Unmanned Aerial Vehicle (UAV)

Barracuda

Tactical Unmanned Aerial Vehicle (UAV)
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Basic Information
Name
Barracuda European Unmanned Aerial Vehicle (UAV)
Designation
Barracuda
Alternate Designation
Barracuda
Equipment Type
Tactical Unmanned Aerial Vehicle (UAV)
Manufacturer
Date of Introduction
2008
Description

The EADS Barracuda is a jet powered European unmanned aerial vehicle (UAV) currently under development by EADS, intended for the role of aerial reconnaissance and also combat (UCAV). The aircraft is a joint venture between Germany and Spain. Development of the project was stopped after the first prototype crashed at sea while approaching for landing during a test flight. The program was resumed in 2008, with a second prototype being completed in November 2008. The rebuilt Barracuda underwent a series of successful flight tests in Goose Bay, Canada during July 2009, followed by further flight campaigns in 2010 and 2012. The Barracuda is primarily in competition with the Dassault nEUROn for strategic and defensive contracts. Both are stealthy and have a maximum air speed of around Mach 0.85. While Germany and Spain are behind the Barracuda, France, Italy, Sweden, Switzerland, Greece, and Spain are funding the nEUROn. Not much is known about the Barracuda as it is still in development; however, it is thought to have an operating ceiling of around 20,000 ft (6,096 m) and carries a maximum payload of 300 kg. The Barracuda is based on commercially available 'off the shelf' components, but also many refined systems. Its fuselage is constructed entirely from carbon fibre, but also has a greater strength to weight ratio than traditional aircraft materials such as Aluminum (the structure of the Eurofighter Typhoon and Boeing 787 Dreamliner are also made significantly out of it). The only significant metal component is the wing spar, running through the middle and reinforcing the wings. The wing spar allows for easy removal of the wings for transportation. The Barracuda uses a specially shaped fuselage, including S-duct air inlet and V-tail, to scatter deflected radar, rendering the UCAV stealthy.

Air & Air Defense Specifications
Engine Turbofan (3190 hp)
Max Speed 0.8 km/h
Wingspan 7.00 m
System
Alternate Designation Barracuda
Type UAV
Dimensions
Length 8.0 m
Wingspan 7.0 m
Empty Vehicle Weight 3,000 kg
Payload 300 kg
Max Takeoff Weight 3,250 kg
Automotive
Engine Name 1 P&W Canada JT15D-5C
Engine Type turbofan engine
Engine Power 3,190 lb (14.2 kN) static thrust
Maximum Speed Mach 0.8
Maximum Distance 200 km
Maximum Altitude 40,000 ft (12,200 m)
Armament
Note None
Protection
Note The Barracuda uses a specially shaped fuselage, including S-duct air inlet and V-tail, to scatter deflected radar, rendering the UCAV stealthy.
Details
Country of Origin Germany
Category Very Low-Cost, Close-Range UAVs (Less than 5 km Range)
Air > Very Low-Cost, Close-Range UAVs (Less than 5 km Range)
Filter Label
B
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
8 m
Width
Height
Weight
3250 kg
Operators (2)
Germany
Spain
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