Photos from the personal collection of Konstantinos Panitsidis
Technical specifications
Photos
Video
A unique multi-role Unmanned Aerial Vehicle System (UAV) with special design to fulfill a plethora of military and civilian operational needs. The innovative Tilt Rotor design coupled with a powerful hybrid power plan system combines the majority of the advantages of a fixed-wing aircraft and a helicopter and ensures a maximum payload of 20 kg.
Multi-role capabilities: Military
-Target Surveillance and Recognition
-Small Explosives Drop
-Armor Supply
-Battle Damage Assessment
-Foreign Aircraft Flight Obstruction
Civil
-Region Surveillance
-Fast Object Transport
-Aero Photography
Agriculture
-Surveying
-Crop Health Monitoring
-Soil Sampling and Analysis
Security
-Border Surveillance
-Suspicious Activity Detection and Tracking
-Area Control & Command
Search and rescue
-Search and Rescue Assistance
-Disaster Assessment
-Medical Assistance
-Food and Equipment Transport
Research
-Weather Monitoring
-Sensor Data
Design characteristics
Modified Riblett Airfoil for Optimum Performance
High Lift Devices For Low Stall Speed
Hybrid (Batter/Fuel) Power Plant For Maximum Range and Endurance
V-Tail Section For Optimum Maneuverability
Power Twin Motor-Propeller Power Plant
Auto pilot, 3-Axis Angular Rate and Acceleration Measurement, GPS update
Loss Link, Loss GPS and Low Battery Failsafe
Sensors: Barometer, Airspeed, External Magnetometer, GPS Receiver, Outside Temperature Sensor and Ultrasonic (or Laser) Altimeter.
Model may be upscaled or downsized according to market needs.
Extra equipment / payload capabilities
Uniform payload compartment
High resolution camera
Payload carrying crane
Real time data transfer
Video recording equipment
Remote control equipment (telemetry)
Mission equipment modular design.
TECHNICAL SPECIFICATIONS
DESIGNER
|
Aviatec S.A.
|
COUNTRY
|
Greece
|
TYPE
|
-
|
POWER-PLANT | Two engine |
Power h.p. | - |
DIMENSIONS
|
|
Length, m
|
3,00
|
Height, m
|
-
|
Wing span, m
|
2,2
|
Wing area, m2
|
-
|
WEIGHT
|
|
Empty aircraft, kg
|
-
|
Normal take-off, kg |
-
|
Maximum take-off, kg |
-
|
Payload, kg | 20 |
PERFORMANCE
|
|
Maximum speed, km/h
|
220
|
Cruising speed, km/h | 180 |
Service ceiling, m
|
-
|
Flight endurance, hour | 7 |
ARMAMENT | - |
PHOTOS Sparrow TILT rotor UAV