TAI ANKA UAV

•Service Ceiling: 30,000 ft
•Endurance: 24 hrs
•Cruise Speed: >75 kts
•Environmental Conditions: 15 kts side wind, 20 kts head wind; temperature, humidity, rain and icing limits as defined in MIL-HDBK-310


System Definition:
With ANKA system, which is developed for day and night real time image intelligence for surveillance, reconnaissance, fixed/moving target detection, identification and tracking missions; the following payload can be carried on board:
•Electro-Optical Day Camera (EO Day TV),
•Day Camera (EO-Electro Optic) / Thermal Camera (IR-Infrared) / LRF-Laser Range Finder & LD-Laser Designator and Spotter,
•SAR-Synthetic Aperture Radar / MTI- Moving Target Indicator & ISAR-Inverse SAR.
Full composite airframe is composed of monocock fuselage, detachable wing and V-Tail, retractable landing gear, equipment bays, service doors and other structural components. The air vehicle is powered by a pusher type piston-prop propulsion system. The airframe is equipped with miscellaneous sub systems like fuel system; de/anti-ice devices; environmental conditioning system for cooling/heating requirements of the compartments.
The avionics system includes a Flight Management System (FMS); integrated to FMS, flight sensors (pitot-static sensor, embedded GPS/INS, magnetic heading, displacement, temperature, pressure transducers), actuators; dedicated communication and identification devices; mission control, record; and other control and interface units.