Specifications | |
Builder team : |
Drone CL 289 : Bombardier, DASA Dornier, Sagem PIVER ground system : Aerospatiale Matra |
In-service in the French Army : |
1993 |
Breadth / Length : |
1.32 m / 3.61 m |
Weight : |
220 kg |
Autonomy : |
30 min / 170 km radius |
Power plant : |
Turbo jet engine |
Maximum speed : |
720 kph |
Navigation : |
Programmed trajectory (inertial guidance, altimetry, doppler) |
Payload : |
Stereoscopic camera, infrared analyser, flight recorder, real time transmission of images from the infrared analyser to ground operators, from up to 70 km |
Composition of the complete system : |
PIVER system : programming and interpretation of reconnaissance devices flights 1 launching and programming unit and 1 or several drones Possible use of heliborne pods instead of drones, with the same sensors |
Major operational capabilities : |
Medium range night and day surveillance of the battlefield by photographic and infrared cameras Real time analysis of infrared images Operational even in very poor weather conditions |
Main user countries : |
Germany |
French Army inventory : |
55 drones en 4 units |
Typical mission |
30-mn 400-km flights at very low altitude allowing rapid and detailed evaluation of targets with transmission of high quality digital images |