Vehicle

TAI Martı

Military Aircraft

The TAI Martı is a small radio-controlled surveillance drone designed, developed and built by Turkish Aerospace Industries in 2003. Its name is the Turkish word for seagull. The shoulder-winged aircraft has an all-composite airframe and a two-cylinder two-stroke gasoline engine of about 1.3 to 1.6 kilowatts in a tractor layout, and it weighs 12 kilograms at maximum take-off. It carries a two-axis gimbaled electro-optical and infrared camera with real-time telemetry, takes off on wheels or by catapult and recovers on wheels or by parachute. It was produced originally for pilot training and has been in service since 2003, and in 2004 it completed aerial image retrieval and shooting tests in Mersin, in work with the Scientific and Technological Research Council of Turkey, that led to replacing an older retrieval system that used balloons.

Facts
Year
2003 1
Propulsion
Petrol 1
Engine Class
Piston 1
Status
In service 1
Top Speed (km/h)
100 1
Maximum Mass (kg)
12 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source TAI Martı (Wikipedia)

Of Make

Source TAI Martı (Wikipedia)
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Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source TAI Martı (Wikipedia)Lead, builder
Quote, Lead, builder
designed, developed and built by Turkish Aerospace Industries (TAI) in 2003

Originated In

Also in Geography Atlas: where this subject originated.

Source TAI Martı (Wikipedia)Lead, builder
Quote, Lead, builder
designed, developed and built by Turkish Aerospace Industries (TAI) in 2003
Sources
1. TAI Martı (Wikipedia)
  • Lead, year of build
    designed, developed and built by Turkish Aerospace Industries (TAI) in 2003
  • Development
    is in service since 2003
  • Lead
    surveillance unmanned drone designed, developed and built by Turkish Aerospace Industries (TAI)
  • Development, powerplant
    propelled by a 2-cylinder 2-stroke gasoline engine of type OS MAX 46 FXi
  • Specifications, maximum take-off weight
    Max takeoff weight: 12 kg (26 lb)
  • Specifications, maximum speed
    Maximum speed: 100 km/h (62 mph, 54 kn)
  • Lead, builder
    designed, developed and built by Turkish Aerospace Industries (TAI) in 2003
  • Exemplifies: Aviation, Lead, type of aircraft
    surveillance unmanned drone designed, developed and built by Turkish Aerospace Industries (TAI)
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