2. Unmanned air vehicle (UAV)

• Flying Wing type.
• Wingspan: 3,10 m.
• Length: 1,23 m.
• Weight at take-off (maximum): 19 Kg.
• Fuselage section: 0,2 m
• Engine: 2 stroke internal-combustion engine. (Power: 2,75 HP/2 Kw.)
• Fuel: gasoline and oil mix. Tank capacity: 6,5 l.
• Speed rank: 60 to 150 Km/h. Cruising speed of 100Km/h
• Endurance: 8 hours. 800 Km of distance at cruising speed with full payload.
• Maximum height: 3.400m
• Take-off with elastic launcher with rubbers.
• Ground Landing: on a spread out net. No needed landing runway.
• Sea Landing: on a pneumatic skate. Waterproof UAV. Satellite radio beacon incorporated in teh UAV for recovering.
• Autopilot with redundant data sources: GPS and inertial navigation. Automatic switching between sources. Tolerant to GPS data failures.
• Flight plan pre-programmed. Possibility to change flight plan during the flight.
• Security routines pre-programmmed for forced landings (lack of communications, gasoline, or engine failures).
• Data link with the control station at 900 Mhz. within 100Km. of distance.
• Real time video link at 2,4Ghz, within 50Km of distance.
• Payload: electro-optical, infrared or photo cameras.
• Electro-optical video camera: 440.000 pixels of resolution. 18x zoom.
• Infrared video camera: 20.480 pixels of resolution. No zoom.
• Spectral response from 900 to 1.700 nm.
• Still image cameras can be optionally mounted.
• Two-axis gyro stabilizad gimbal.
• Point our of targets.