Vehicle

TAI Anka

Military Aircraft

The TAI Anka is a family of medium-altitude long-endurance unmanned aerial vehicles developed by Turkish Aerospace Industries for the Turkish Air Force and for export. It is named after the Anka, the Turkish name of the mythical phoenix, and grew out of a development contract that took effect on 24 December 2004. The first prototype flew on 30 December 2010, the Anka-B version made its first flight in 2014, and in 2017 the Anka-S was introduced and entered service with the Turkish Air Force. A system consists of air vehicles, a ground control station and an automatic take-off and landing system, and the aircraft carries electro-optic sensors and a synthetic-aperture radar for intelligence, surveillance and reconnaissance, with variants for electronic warfare, signals intelligence and carrying precision munitions. It shares a common avionics architecture and ground segment with the Anka-3 and the Aksungur.

Facts
Year
2010 1
Propulsion
Diesel 1
Status
In service 1
Top Speed (km/h)
217 1
Maximum Mass (kg)
1700 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source TAI Anka (Wikipedia)

Of Make

Source TAI Anka (Wikipedia)
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Manufactured By

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Source TAI Anka (Wikipedia)Lead, builder
Quote, Lead, builder
developed by Turkish Aerospace Industries for the Turkish Air Force and export

Originated In

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Source TAI Anka (Wikipedia)Lead, builder
Quote, Lead, builder
developed by Turkish Aerospace Industries for the Turkish Air Force and export
Sources
1. TAI Anka (Wikipedia)
  • Development, first flight
    On 30 December 2010, the first TAI Anka unmanned aerial vehicle completed its debut flight
  • Lead
    In 2017, Turkish Aerospace Industries introduced Anka-S and the aircraft entered service with the Turkish Air Force
  • Lead, body style
    is a family of medium-altitude long-endurance unmanned aerial vehicles developed by Turkish Aerospace Industries
  • Specifications (Anka-S), fuel type
    Fuel type: Diesel and JP-8 jet fuel
  • Specifications (Anka-S), maximum take-off mass
    Max. take-off mass: 1,700 kg (3,750 lb)
  • Specifications (Anka-S), maximum speed
    Maximum speed: ~217 km/h (117 kn; 135 mph)
  • Lead, builder
    developed by Turkish Aerospace Industries for the Turkish Air Force and export
  • Exemplifies: Aviation, Lead, type of aircraft
    is a family of medium-altitude long-endurance unmanned aerial vehicles developed by Turkish Aerospace Industries
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