TAI

Manufacturer:

TAI

Country:

Turkey

Commercial designation:

Mangusta

Technical designation:

T129

Version, Variant:

Export

Type:

Conventional

Currently produced:

Y

Typical missions:

Military Combat Attack

Flight conditions:

IFR

First flight:

2009

Landing system:

wheels

Blades number:

5

Tail blades number:

2

MTOW with external loads:

5100 kg

11245.5 lbs

MTOW with only internal loading:

0 kg

0 lbs

Empty weight:

0 kg

0 lbs

External payload:

0 kg

0 lbs

Internal payload:

0 kg

0 lbs

Standard fuel tank:

0 kg

0 lbs

with optionnal external fuel tank:

0 kg

0 lbs

Cruise speed:

0 km/h

0 kt

Maximum cruise speed:

0 km/h

0 kt

Vne:

269 km/h

145.26 kt

Max negative g @ MTOW:

0 g

Max positive g @ MTOW:

0 g

Range with normal tanks:

561 km

302.94 nm

Max range with auxiliary external tanks:

1000 km

540 nm

Max endurance @ min consumption speed:

03:00:00 h:min

Rate of climb @ SL:

14 m/s

2755.2 ft/min

Rate of climb @ SL @MTOW:

0 m/s

0 ft/min

IGE max hovering altitude, MTOW:

3995 m

13103.6 ft

IGE max hovering altitude, empty:

0 m

0 ft

IGE max hovering altitude, ISA+20°C, MTOW:

0 m

0 ft

IGE max hovering altitude, ISA+20°C, empty:

0 m

0 ft

OGE max hovering altitude, MTOW:

3050 m

10004 ft

OGE max hovering altitude, empty:

0 m

0 ft

OGE max hovering altitude, ISA+20°C, MTOW:

0 m

0 ft

OGE max hovering altitude, ISA+20°C, empty:

0 m

0 ft

Service ceiling ISA, MTOW:

6100 m

20008 ft

Max operating altitude, empty weight:

0 m

0 ft

Highest use Temperature:

0 °C

0 °F

Lowest use Temperature:

0 °C

0 °F

APU in HC:

Engine manufacturer:

LHTEC

Model:

CTS800-4A

Engines quantity:

2

Powerplant category:

turbine

Main rotor rotation speed:

0 rpm

Fuel consumption @ SL @ max continuous speed:

0 kg/kW/h

0 lbs/hp/h

Minimum consumption speed @ SL:

0 km/h

0 kt

Fuel consumption @ eco cruise speed @SL:

0 kg/h

0 lbs/h

Fuel consumption @ min consumption speed @ SL:

0 kg/h

0 lbs/h

Engines nominal power:

2028 kW

2756.052 hp

Transmission shaft max continuous power:

0 kW

0 hp

Transmission shaft max power:

0 kW

0 hp

Takeoff power 5 min:

2760 kW

3750.84 hp

OEI 30s power:

0 kW

0 hp

OEI 2min power:

0 kW

0 hp

OEI max continuous power :

1207 kW

1640.313 hp

OEI max continuous transmission power:

0 kW

0 hp

OEI 30 sec transmission power:

0 kW

0 hp

OEI 2 min transmission power:

0 kW

0 hp

Overall length:

14.55 m

47.724 ft

Rotor diameter:

11.9 m

39.032 ft

Tail rotor diameter:

2.55 m

8.364 ft

Fuselage length:

12.37 m

40.5736 ft

Overall height:

3.96 m

12.9888 ft

Main rotor blades chord:

0 m

0 ft

Tail rotor blades chord:

0 m

0 ft

Mast tilt angle:

0 °

Noise at flyover, level:

0 dB EPNL

Noise at flyover, limit:

0 dB EPNL

Noise at takeoff, level:

0 dB EPNL

Noise at takeoff, limit:

0 dB EPNL

Noise at landing, level:

0 dB EPNL

Noise at landing, limit:

0 dB EPNL

Crew:

2

Max pax number:

0

Average price:

17000000 $