Sperwer-HV  
Initial Operational Capability (IOC): 2004
Total Production: ?
Also Known As: SDTI
Origin: France
Corporations: Sagem Defense Securite
Parent System: Sperwer
Initial Operational Capability (IOC): 2001
Total Production: 130
Family Members: Sperwer and Sperwer B
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Description: The Sperwer, also known as Ugglan in Sweden and CU-161 in Canada, is a modular, low observable, multi-mission, delta-wing unmanned air vehicle (UAV) designed to provide real time Intelligence, Surveillance, Target Acquisition an Reconnaissance (ISTAR) capabilities in support of land forces. Sagem Defense Securite developed this UAV system in response to the French Army's SDTI (Système de Drones Tactiques Intérimaire or Interim Tactical UAV System) program. The Sperwer UAV family offering more than six hours of flight endurance includes the basic version, a high speed low altitude drone variant and a long endurance variant known as Sperwer B.

The Spervwer air vehicle utilizes a vehicle-mounted ramp for taking off and a combination of parachute and airbags for landing. Its payload includes the synthetic aperture radar (SAR), electronic warfare (EW), communications relay or EUROFLIR optronic gimbaled pod that may include daylight CCD-TV sensor, laser designator/rangefinder and/or day/night Infrared imagery sensor. A single Sperwer system includes a ground control station, ground data terminal with the tactical data link, a vehicle integrated with a catapult launcher and air vehicles. The ground control station can control two air vehicles at the same time.

The Sperwer-HV is a turbo-jet powered, high velocity aerial vehicle evolved from the Sperwer air vehicle which was powered by two-cylinder 65-hp engine. The high speed low altitude air vehicle is optimized for deeper, faster and stealthier penetration of enemy airspace. It is fitted with forward-swept wings and canard foreplanes and results far more survivable to enemy fire due to its higher speed. The Sperwer-HV can fly at 10,000 meters of altitude traveling at 400 knots with a mission radius of over 400 km.

Sperwer-HV Specifications

Crew: 0
Number of Engines: 1
Performance
Ceiling: 10,000 meter (32,808 foot)
Max Range: 800 kilometer (432 nautical mile)
Speed
Top Speed at High Altitude: 400 knot (740 kph)
Weight
Payload: 50 kilogram (110 pound)
CEP: Circular Error Probable
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)

Sperwer-HV News

There is 1 news
on 27 Feb 2012
Monday, February 27, 2012Sagem Wins Maintenance Contract for Sperwer Drones Deployed by French Army

Operators & Related Equipment


OperatorsItems

Grand Total ?1
Sensor Systems
EUROFLIRx1
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