NHI

Manufacturer:

NHI

Country:

Europe

Commercial designation:

Caiman

Technical designation:

NH90

Version, Variant:

TTH RR-TM

Type:

Conventional

Currently produced:

Y

Typical missions:

Utility Military Terrestrial

Flight conditions:

IFR

First flight:

0

Landing system:

wheels

Blades number:

4

Tail blades number:

4

MTOW with external loads:

11400 kg

25137 lbs

MTOW with only internal loading:

10600 kg

23373 lbs

Empty weight:

6000 kg

13230 lbs

External payload:

4000 kg

8820 lbs

Internal payload:

4200 kg

9261 lbs

Standard fuel tank:

2035 kg

4487.175 lbs

with optionnal external fuel tank:

3035 kg

6692.175 lbs

Cruise speed:

260 km/h

140.4 kt

Maximum cruise speed:

300 km/h

162 kt

Vne:

300 km/h

162 kt

Max negative g @ MTOW:

0 g

Max positive g @ MTOW:

0 g

Range with normal tanks:

800 km

432 nm

Max range with auxiliary external tanks:

982 km

530.28 nm

Max endurance @ min consumption speed:

05:00:00 h:min

Rate of climb @ SL:

11 m/s

2164.8 ft/min

Rate of climb @ SL @MTOW:

0 m/s

0 ft/min

IGE max hovering altitude, MTOW:

3200 m

10496 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:

2600 m

8528 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:

0 m

0 ft

Max operating altitude, empty weight:

0 m

0 ft

Highest use Temperature:

50 °C

90 °F

Lowest use Temperature:

-40 °C

-72 °F

APU in HC:

Y

Engine manufacturer:

Turbomeca

Model:

RTM-322-01/9

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:

0 kW

0 hp

Transmission shaft max continuous power:

0 kW

0 hp

Transmission shaft max power:

0 kW

0 hp

Takeoff power 5 min:

0 kW

0 hp

OEI 30s power:

0 kW

0 hp

OEI 2min power:

0 kW

0 hp

OEI max continuous power :

0 kW

0 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:

19.56 m

64.1568 ft

Rotor diameter:

16.3 m

53.464 ft

Tail rotor diameter:

3.2 m

10.496 ft

Fuselage length:

16.09 m

52.7752 ft

Overall height:

4.16 m

13.6448 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:

3

Max pax number:

20

Average price:

16000000 $