Tuesday, December 02, 2008

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Sperwer


IOC: 2001

Sperwer-HV


IOC: 2004

Also Known As
SDTI


Origin
France


Contractor/s
Sagem Defense Securite

Family Members
Sperwer
Sperwer-LE

Description: The Sperwer is a low observable, delta-wing Unmanned Aerial Vehicle (UAV) meant for ISTAR (Intelligence, Surveillance, Target Acquisition, and Reconnaissance) missions. It can be equipped with daylight CCD-TV sensor or day/night Infrared imagery sensor. The UAV requires a ramp for the taking off operation and uses a parachute and airbags for landing.

The Sperwer-HV is a turbo-jet powered, high velocity aerial vehicle evolved from Sperwer optimized for deeper, faster and stealthier penetration of enemy airspace. It is being fitted with forward-swept wings with canard foreplanes.

Sperwer-HV can fly at 10,000 meters of altitude traveling at 400 knots with a mission radius of over 400 km. It can be equipped with a synthetic aperture radar as well as electro-optical sensors (EO/IR) or a laser designator.

Specifications
Accommodation: Unmanned

Weights: Payload 50 kg (110 lb)

Performance: Ceiling 10,000 m (32,808 ft), Max Range 800 km (432 nm), Top Speed 206 mps (Mach 0.62)

Other: Number of Engines 1

Operators

France


Image Gallery


Notes
(*) lead contractor
IOC: Initial Operating Capability
FOC: Full Operating Capability
CEP: Circular Error Probable
Comm: Commissioning Date
Meters (m)   Kilometers (km)   Nautic Miles (nm)   Inch (in)   Yard (yd)   Foot (ft)   Millimeter (mm)
Pound (lb)   Kilogram (kg)   kN (KiloNewton)   Ton (t)
Meters per Second (mps)   Kilometers per Hour (kph)   Knot (kt)   Miles per Hour (mph)
Liter (l)   Galon (gl)
Year (yr)   Minutes (min)   Second (sec)
Shaft-Horse-Power (shp)


Last Updated: Saturday, November 22, 2008

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