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Tarkopter_1

TARKOPTER – I

GENERAL

DESCRIPTION

The Tarkopter-I is a multi-purpose gasoline engine-powered helicopter UAV that
can carry up to 30 kg payloads for as long as 2 hrs (10Kg payload for 4 hours).

The flight stages, take-off, hover, flight and landing are done by autonomously.
The Tarkopter-I could be equipped with satCom as commonication link that is for
BVLOS operations. The gasoline engine has advanced cooling system that ensures
reliable operations in hot and moist enviorenment.

Tarkopter-I’s unique capability, multipayload option, enables carrying upto three
gimbal that enables Wide Area Surveliance in one platform, by focusing 3
simultaneous events at same time.

APPLICATION

AREAS

  • Agrochemical spraying
  • Radio Relay
  • Surveliance of
    • Marine
    • Environment
    • Critical infrastructure
    • Critical infrastructure

KEY

FEATURES

 

  • Daylight HD video Sensor
  • LWIR/MWIR Night vision sensor
  • Multi/Hyper spectral sensor
  • Gigapixel camera for photogrametry
  • Transponder ADS-B
  • Lidar
  • RF date link at 2.2-2.4Ghz

DIMENSION

tarkopter_boyut

SPECIFICATION

Cruising speed 70 Km/h
Maximum speed 100 Km/h
Length 2500 mm
Main rotor diameter 3100 mm
Height 952 mm
Engine type 4 stroke rotary
Fuel feed Carburated
Power 30 kW
Max. payload 30 Kg
MTOW 110 Kg
Empty weight 60 Kg
Fuel tank (max) 40 lt
Average fuel consumption 5-9 lt/hour
Max. climbing capacity 3 m/sn
Max. wind speed during taking off or landing 12 m/sn
Practical range 350 km
Practical celling 3500 m
Flight time (max with 12 kg payload) 5 hours
Parachute Ballistic optiona
Onboard power supply 300W 12-24Volt
Battery type (included) Li-Fe
Altimetre Lazer/Milimetre dalga radar
TBI (planned maintenance) 250 Saat
On board generator

600W
Power Distirbution 300W 12-24Volt
Temperature range -20°C to +45°C
Base 15×15 port
Control modes Autonomous
Semi-autonomous
Emergency
Takeoff and landing Autonomous
Emergency landing Parachute
Ground landing equipment None
Engine start Onboard starter