Tuesday, December 02, 2008

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Sperwer


IOC: 2001

Sperwer-LE


IOC: 2004

Also Known As
SDTI


Origin
France


Contractor/s
Sagem Defense Securite

Family Members
Sperwer
Sperwer-HV

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 catapult/ramp for the taking off operation and uses a parachute and airbags for landing.

The Sperwer-LE is intended for long endurance loitering missions at medium altitude. It features a clipped delta wing high-lift design with a payload capacity of 50 kg for Synthetic Aperture Radar (RADAR) or electro-optical sensors (EO/IR). This UAV is fully compatible with Sperwer control station and launch catapult.

Specifications
Accommodation: Unmanned

Weights: Payload 50 kg (110 lb)

Performance: Ceiling 6,100 m (20,013 ft), Endurance 12 hours

Other: Number of Engines 1

News

 

Operators

France

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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