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Cougar AS532 SC

Airbus Helicopters Military Range - Cougar AS532 SC
aircraft
Manufacturer:
Airbus Helicopters
Country:
Europe
Commercial designation:
Cougar
Technical designation:
AS532
Version, Variant:
SC
Type:
Conventional
Currently produced:
Y
Typical missions:
Military Naval Combat
Flight conditions:
First flight:
1990
Landing system:
wheels
Blades number:
4
Tail blades number:
0
weight
Weight class:
4
MTOW with external loads:
0 kg0 lbs
MTOW with only internal loading:
0 kg0 lbs
Empty weight:
0 kg0 lbs
External payload:
0 kg0 lbs
Internal payload:
0 kg0 lbs
Standard fuel tank:
0 kg0 lbs
with optionnal external fuel tank:
0 kg0 lbs
performance
Cruise speed:
0 km/h0 kt
Maximum cruise speed:
0 km/h0 kt
Vne:
0 km/h0 kt
Max negative g @ MTOW:
0 g
Max positive g @ MTOW:
0 g
Range with normal tanks:
0 km0 nm
Max range with auxiliary external tanks:
0 km0 nm
Max endurance @ min consumption speed:
00:00:00 h:min
Rate of climb @ SL:
0 m/s0 ft/min
Rate of climb @ SL @MTOW:
0 m/s0 ft/min
IGE max hovering altitude, MTOW:
0 m0 ft
IGE max hovering altitude, empty:
0 m0 ft
IGE max hovering altitude, ISA+20°C, MTOW:
0 m0 ft
IGE max hovering altitude, ISA+20°C, empty:
0 m0 ft
OGE max hovering altitude, MTOW:
0 m0 ft
OGE max hovering altitude, empty:
0 m0 ft
OGE max hovering altitude, ISA+20°C, MTOW:
0 m0 ft
OGE max hovering altitude, ISA+20°C, empty:
0 m0 ft
Service ceiling ISA, MTOW:
0 m0 ft
Max operating altitude, empty weight:
0 m0 ft
Highest use Temperature:
0 °C0 °F
Lowest use Temperature:
0 °C0 °F
power
APU in HC:
Engine manufacturer:
Model:
Engines quantity:
0
Powerplant category:
turbine
Main rotor rotation speed:
0 rpm
Fuel consumption @ SL @ max continuous speed:
0 kg/kW/h0 lbs/hp/h
Minimum consumption speed @ SL:
0 km/h0 kt
Fuel consumption @ eco cruise speed @SL:
0 kg/h0 lbs/h
Fuel consumption @ min consumption speed @ SL:
0 kg/h0 lbs/h
Engines nominal power:
0 kW0 hp
Transmission shaft max continuous power:
0 kW0 hp
Transmission shaft max power:
0 kW0 hp
Takeoff power 5 min:
0 kW0 hp
OEI 30s power:
0 kW0 hp
OEI 2min power:
0 kW0 hp
OEI max continuous power :
0 kW0 hp
OEI max continuous transmission power:
0 kW0 hp
OEI 30 sec transmission power:
0 kW0 hp
OEI 2 min transmission power:
0 kW0 hp
dimensions
Overall length:
0 m0 ft
Rotor diameter:
0 m0 ft
Tail rotor diameter:
0 m0 ft
Fuselage length:
0 m0 ft
Overall height:
0 m0 ft
Main rotor blades chord:
0 m0 ft
Tail rotor blades chord:
0 m0 ft
Mast tilt angle:
0 °
noise
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
seating
Crew:
0
Max pax number:
0
use
Average price:
0 $
Read more »
Label:

Cougar AS532 M

Airbus Helicopters Military Range - Cougar AS532 M
aircraft
Manufacturer:
Airbus Helicopters
Country:
Europe
Commercial designation:
Cougar
Technical designation:
AS532
Version, Variant:
M
Type:
Currently produced:
Typical missions:
Flight conditions:
First flight:
0
Landing system:
Blades number:
0
Tail blades number:
0
weight
Weight class:
0
MTOW with external loads:
0 kg0 lbs
MTOW with only internal loading:
0 kg0 lbs
Empty weight:
0 kg0 lbs
External payload:
0 kg0 lbs
Internal payload:
0 kg0 lbs
Standard fuel tank:
0 kg0 lbs
with optionnal external fuel tank:
0 kg0 lbs
performance
Cruise speed:
0 km/h0 kt
Maximum cruise speed:
0 km/h0 kt
Vne:
0 km/h0 kt
Max negative g @ MTOW:
0 g
Max positive g @ MTOW:
0 g
Range with normal tanks:
0 km0 nm
Max range with auxiliary external tanks:
0 km0 nm
Max endurance @ min consumption speed:
00:00:00 h:min
Rate of climb @ SL:
0 m/s0 ft/min
Rate of climb @ SL @MTOW:
0 m/s0 ft/min
IGE max hovering altitude, MTOW:
0 m0 ft
IGE max hovering altitude, empty:
0 m0 ft
IGE max hovering altitude, ISA+20°C, MTOW:
0 m0 ft
IGE max hovering altitude, ISA+20°C, empty:
0 m0 ft
OGE max hovering altitude, MTOW:
0 m0 ft
OGE max hovering altitude, empty:
0 m0 ft
OGE max hovering altitude, ISA+20°C, MTOW:
0 m0 ft
OGE max hovering altitude, ISA+20°C, empty:
0 m0 ft
Service ceiling ISA, MTOW:
0 m0 ft
Max operating altitude, empty weight:
0 m0 ft
Highest use Temperature:
0 °C0 °F
Lowest use Temperature:
0 °C0 °F
power
APU in HC:
Engine manufacturer:
Model:
Engines quantity:
0
Powerplant category:
Main rotor rotation speed:
0 rpm
Fuel consumption @ SL @ max continuous speed:
0 kg/kW/h0 lbs/hp/h
Minimum consumption speed @ SL:
0 km/h0 kt
Fuel consumption @ eco cruise speed @SL:
0 kg/h0 lbs/h
Fuel consumption @ min consumption speed @ SL:
0 kg/h0 lbs/h
Engines nominal power:
0 kW0 hp
Transmission shaft max continuous power:
0 kW0 hp
Transmission shaft max power:
0 kW0 hp
Takeoff power 5 min:
0 kW0 hp
OEI 30s power:
0 kW0 hp
OEI 2min power:
0 kW0 hp
OEI max continuous power :
0 kW0 hp
OEI max continuous transmission power:
0 kW0 hp
OEI 30 sec transmission power:
0 kW0 hp
OEI 2 min transmission power:
0 kW0 hp
dimensions
Overall length:
0 m0 ft
Rotor diameter:
0 m0 ft
Tail rotor diameter:
0 m0 ft
Fuselage length:
0 m0 ft
Overall height:
0 m0 ft
Main rotor blades chord:
0 m0 ft
Tail rotor blades chord:
0 m0 ft
Mast tilt angle:
0 °
noise
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
seating
Crew:
0
Max pax number:
0
use
Average price:
0 $
Read more »
Label:

Cougar AS532 AL

Airbus Helicopters Military Range - Cougar AS532 AL
aircraft
Manufacturer:
Airbus Helicopters
Country:
Europe
Commercial designation:
Cougar
Technical designation:
AS532
Version, Variant:
AL
Type:
Conventional
Currently produced:
Y
Typical missions:
Military Terrestrial Utility Combat
Flight conditions:
First flight:
0
Landing system:
wheels
Blades number:
4
Tail blades number:
0
weight
Weight class:
4
MTOW with external loads:
9350 kg20617 lbs
MTOW with only internal loading:
9000 kg19845 lbs
Empty weight:
4610 kg10165 lbs
External payload:
4500 kg9923 lbs
Internal payload:
4930 kg10871 lbs
Standard fuel tank:
0 kg0 lbs
with optionnal external fuel tank:
0 kg0 lbs
performance
Cruise speed:
0 km/h0 kt
Maximum cruise speed:
258 km/h139 kt
Vne:
278 km/h150 kt
Max negative g @ MTOW:
0 g
Max positive g @ MTOW:
0 g
Range with normal tanks:
776 km419 nm
Max range with auxiliary external tanks:
0 km0 nm
Max endurance @ min consumption speed:
00:00:00 h:min
Rate of climb @ SL:
7.2 m/s1417 ft/min
Rate of climb @ SL @MTOW:
0 m/s0 ft/min
IGE max hovering altitude, MTOW:
2800 m9184 ft
IGE max hovering altitude, empty:
0 m0 ft
IGE max hovering altitude, ISA+20°C, MTOW:
0 m0 ft
IGE max hovering altitude, ISA+20°C, empty:
0 m0 ft
OGE max hovering altitude, MTOW:
1650 m5412 ft
OGE max hovering altitude, empty:
0 m0 ft
OGE max hovering altitude, ISA+20°C, MTOW:
0 m0 ft
OGE max hovering altitude, ISA+20°C, empty:
0 m0 ft
Service ceiling ISA, MTOW:
3450 m11316 ft
Max operating altitude, empty weight:
0 m0 ft
Highest use Temperature:
0 °C0 °F
Lowest use Temperature:
0 °C0 °F
power
APU in HC:
Engine manufacturer:
Model:
Engines quantity:
2
Powerplant category:
turbine
Main rotor rotation speed:
0 rpm
Fuel consumption @ SL @ max continuous speed:
0 kg/kW/h0 lbs/hp/h
Minimum consumption speed @ SL:
0 km/h0 kt
Fuel consumption @ eco cruise speed @SL:
0 kg/h0 lbs/h
Fuel consumption @ min consumption speed @ SL:
0 kg/h0 lbs/h
Engines nominal power:
2370 kW3221 hp
Transmission shaft max continuous power:
0 kW0 hp
Transmission shaft max power:
0 kW0 hp
Takeoff power 5 min:
2714 kW3688 hp
OEI 30s power:
1400 kW1903 hp
OEI 2min power:
1330 kW1807 hp
OEI max continuous power :
0 kW0 hp
OEI max continuous transmission power:
0 kW0 hp
OEI 30 sec transmission power:
0 kW0 hp
OEI 2 min transmission power:
0 kW0 hp
dimensions
Overall length:
0 m0 ft
Rotor diameter:
0 m0 ft
Tail rotor diameter:
0 m0 ft
Fuselage length:
0 m0 ft
Overall height:
0 m0 ft
Main rotor blades chord:
0 m0 ft
Tail rotor blades chord:
0 m0 ft
Mast tilt angle:
0 °
noise
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
seating
Crew:
0
Max pax number:
0
use
Average price:
0 $
Read more »
Label:

Cougar AS532 AC

Airbus Helicopters Military Range - Cougar AS532 AC
aircraft
Manufacturer:
Airbus Helicopters
Country:
Europe
Commercial designation:
Cougar
Technical designation:
AS532
Version, Variant:
AC
Type:
Currently produced:
Typical missions:
Flight conditions:
First flight:
0
Landing system:
Blades number:
0
Tail blades number:
0
weight
Weight class:
0
MTOW with external loads:
0 kg0 lbs
MTOW with only internal loading:
0 kg0 lbs
Empty weight:
0 kg0 lbs
External payload:
0 kg0 lbs
Internal payload:
0 kg0 lbs
Standard fuel tank:
0 kg0 lbs
with optionnal external fuel tank:
0 kg0 lbs
performance
Cruise speed:
0 km/h0 kt
Maximum cruise speed:
0 km/h0 kt
Vne:
0 km/h0 kt
Max negative g @ MTOW:
0 g
Max positive g @ MTOW:
0 g
Range with normal tanks:
0 km0 nm
Max range with auxiliary external tanks:
0 km0 nm
Max endurance @ min consumption speed:
00:00:00 h:min
Rate of climb @ SL:
0 m/s0 ft/min
Rate of climb @ SL @MTOW:
0 m/s0 ft/min
IGE max hovering altitude, MTOW:
0 m0 ft
IGE max hovering altitude, empty:
0 m0 ft
IGE max hovering altitude, ISA+20°C, MTOW:
0 m0 ft
IGE max hovering altitude, ISA+20°C, empty:
0 m0 ft
OGE max hovering altitude, MTOW:
0 m0 ft
OGE max hovering altitude, empty:
0 m0 ft
OGE max hovering altitude, ISA+20°C, MTOW:
0 m0 ft
OGE max hovering altitude, ISA+20°C, empty:
0 m0 ft
Service ceiling ISA, MTOW:
0 m0 ft
Max operating altitude, empty weight:
0 m0 ft
Highest use Temperature:
0 °C0 °F
Lowest use Temperature:
0 °C0 °F
power
APU in HC:
Engine manufacturer:
Model:
Engines quantity:
0
Powerplant category:
Main rotor rotation speed:
0 rpm
Fuel consumption @ SL @ max continuous speed:
0 kg/kW/h0 lbs/hp/h
Minimum consumption speed @ SL:
0 km/h0 kt
Fuel consumption @ eco cruise speed @SL:
0 kg/h0 lbs/h
Fuel consumption @ min consumption speed @ SL:
0 kg/h0 lbs/h
Engines nominal power:
0 kW0 hp
Transmission shaft max continuous power:
0 kW0 hp
Transmission shaft max power:
0 kW0 hp
Takeoff power 5 min:
0 kW0 hp
OEI 30s power:
0 kW0 hp
OEI 2min power:
0 kW0 hp
OEI max continuous power :
0 kW0 hp
OEI max continuous transmission power:
0 kW0 hp
OEI 30 sec transmission power:
0 kW0 hp
OEI 2 min transmission power:
0 kW0 hp
dimensions
Overall length:
0 m0 ft
Rotor diameter:
0 m0 ft
Tail rotor diameter:
0 m0 ft
Fuselage length:
0 m0 ft
Overall height:
0 m0 ft
Main rotor blades chord:
0 m0 ft
Tail rotor blades chord:
0 m0 ft
Mast tilt angle:
0 °
noise
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
seating
Crew:
0
Max pax number:
0
use
Average price:
0 $
Read more »
Label:

Airbus Helicopters Military Range - Tiger

Airbus Helicopters Military Range - Tiger
The Airbus Helicopters (formerly Eurocopter Group) is a global helicopter manufacturing and support company. It is the largest in the industry in terms of revenues and turbine helicopter deliveries. Its head office is located on the property of Marseille-Provence International Airport in Marignane, France, near Marseille. Airbus Helicopters's main facilities are at its headquarters in Marignane in France, at Eurocopter Deutschland GmbH in Donauwörth, Germany and at Eurocopter España in Albacete, Spain. The company was renamed Airbus Helicopters on 2 January 2014.

Characteristics

Characteristics
TYPICAL CHARACTERISTICS
Maxi Take-Off Weight (MTOW) - ISA, SL
6,600 kg
14,553 lb
Engine 2 x MTR 390 - Step 1-5
1,092 kW
1,464 shp
Super contingency power (OEI)
1,322 kW 1,774 shp
Standard fuel capacity
1,105 kg 2,435 lb
Standard fuel capacity + external fuel tanks 1,689 kg 3,723 lb

PERFORMANCES
Fast cruise speed at MTOW SL
271 km/h
146 kts
Mission duration (standard)
2 h 30 min
Maximum endurance with external fuel tank
5 h 00 min
Max range “armed” with standard fuel tanks 400 nm 740 km
Max range “not armed” with external fuel tanks 610 nm 1,130 km

FLIGHT ENVELOPE
Operating temperature
- 30°C to ISA + 35°C
Service ceiling -500 m to 4000 m -1,640 ft to 13,123 ft



  • Typical configurations


    TechnologiesAttack
    • 4 Air-to-Air Mistral
      + 8 Hellfire or Spike
      + 30mm turreted gun




    TechnologiesGround
    • 68 rockets 68mm
    or
    • 52 rockets 70mm
      + 30mm turreted gun

    Technologies
    Attack

    • 2 Air-to-Air Mistral
      + 4 Hellfire or Spike
      + 34 rockets 68mm
    or
    • 26 rockets 70mm
      + 30mm turreted gun  


    Technologies
    Armed Reconnaissance
    • 4 Air-to-Air Mistral
      + 44 rockets 68mm
    or
    • 38 rockets 70mm
      + 30mm turreted gun


    Technologies
    Air-to-Air combat
    • 4 Air-to-Air Mistral
      + 30mm turreted gun


Cockpit & Avionics

  • Tandem, pilot in frontTechnologies
  • Air conditioned
  • Redundant MIL 1553 data bus
  • Glass cockpit (4 displays)
  • Map Display with battlefield
    management system
  • Satellite, HF and VHF/FM
    data transfer
  • Radar, laser, missile launch warning
    and chaff/flares dispenser





Survivability

  • Low radar signature
  • Low infrared emission
  • Outstanding aircraft agility

Missions
LRU exchange in NBC Conditions
(ARINC 600


Mission System

Gyro stabilized Roof Mounted Sight (RMS)          MissionsMissions
  • TV camera (3 FoV),
  • Thermal imager (3 FoV + electronic Zoom),
  • Laser range finder,
  • Laser designator,
  • Laser spot tracker, up to 4 targets automatic tracker.
  • Steered in azimuth (+/- 120°) and elevation (+40°/-25°).


Helmet-Mounted Sight/Displays (HMSD)          MissionsMissions
  • Pilot’s and Gunner’s
  • Piloting and firing symbology.
  • Slaving function,either with RMS or with 30 mm turret-mounted gun.
 Missions
Digital Map Generator
  • System EUROGRID
  • Map display
  • Battlefield management system

IFF Transponder / Interrogator

HF/Datalink
    Missions
  • Topographical maps,
  • IFR charts,
  • Mission overlays,
  • Presentation of target photos,
  • Recording and display of IR/TV sensor images of Gunner sight,
  • Target hand-over,
  • Radio data link managements,
  • Handling of mission data.


  • Services

    Training


    • On board training device
    • 3 videos + 1 audio recorded









Read more »
Label:

Tiger EC665 UHT

 Airbus Helicopters Military Range - Tiger EC665 UHT
aircraft
Manufacturer:
Airbus Helicopters
Country:
Europe
Commercial designation:
Tiger
Technical designation:
EC665
Version, Variant:
UHT
Type:
Conventional
Currently produced:
Y
Typical missions:
Military Combat Attack
Flight conditions:
IFR
First flight:
1991
Landing system:
wheels
Blades number:
4
Tail blades number:
3
weight
Weight class:
4
MTOW with external loads:
6100 kg13451 lbs
MTOW with only internal loading:
0 kg0 lbs
Empty weight:
4350 kg9592 lbs
External payload:
1650 kg3638 lbs
Internal payload:
0 kg0 lbs
Standard fuel tank:
1105 kg2437 lbs
with optionnal external fuel tank:
1689 kg3724 lbs
performance
Cruise speed:
230 km/h124 kt
Maximum cruise speed:
259 km/h140 kt
Vne:
298 km/h161 kt
Max negative g @ MTOW:
0 g
Max positive g @ MTOW:
0 g
Range with normal tanks:
800 km432 nm
Max range with auxiliary external tanks:
1280 km691 nm
Max endurance @ min consumption speed:
03:25:00 h:min
Rate of climb @ SL:
10.7 m/s2106 ft/min
Rate of climb @ SL @MTOW:
0 m/s0 ft/min
IGE max hovering altitude, MTOW:
0 m0 ft
IGE max hovering altitude, empty:
0 m0 ft
IGE max hovering altitude, ISA+20°C, MTOW:
0 m0 ft
IGE max hovering altitude, ISA+20°C, empty:
0 m0 ft
OGE max hovering altitude, MTOW:
3200 m10496 ft
OGE max hovering altitude, empty:
0 m0 ft
OGE max hovering altitude, ISA+20°C, MTOW:
0 m0 ft
OGE max hovering altitude, ISA+20°C, empty:
0 m0 ft
Service ceiling ISA, MTOW:
4000 m13120 ft
Max operating altitude, empty weight:
0 m0 ft
Highest use Temperature:
35 °C63 °F
Lowest use Temperature:
-30 °C-54 °F
power
APU in HC:
Engine manufacturer:
Turbomeca
Model:
MTR 390
Engines quantity:
2
Powerplant category:
turbine
Main rotor rotation speed:
0 rpm
Fuel consumption @ SL @ max continuous speed:
0 kg/kW/h0 lbs/hp/h
Minimum consumption speed @ SL:
0 km/h0 kt
Fuel consumption @ eco cruise speed @SL:
0 kg/h0 lbs/h
Fuel consumption @ min consumption speed @ SL:
0 kg/h0 lbs/h
Engines nominal power:
1746 kW2373 hp
Transmission shaft max continuous power:
0 kW0 hp
Transmission shaft max power:
0 kW0 hp
Takeoff power 5 min:
1936 kW2631 hp
OEI 30s power:
1160 kW1576 hp
OEI 2min power:
0 kW0 hp
OEI max continuous power :
0 kW0 hp
OEI max continuous transmission power:
0 kW0 hp
OEI 30 sec transmission power:
0 kW0 hp
OEI 2 min transmission power:
0 kW0 hp
dimensions
Overall length:
15.82 m52 ft
Rotor diameter:
13 m43 ft
Tail rotor diameter:
2.7 m9 ft
Fuselage length:
14.27 m47 ft
Overall height:
5.2 m17 ft
Main rotor blades chord:
0 m0 ft
Tail rotor blades chord:
0 m0 ft
Mast tilt angle:
0 °
noise
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
seating
Crew:
2
Max pax number:
0
use
Average price:
3.2e+07 $
Read more »
Label:

Tiger EC665 HAP

 Airbus Helicopters Military Range - Tiger EC665 HAP
aircraft
Manufacturer:
Airbus Helicopters
Country:
Europe
Commercial designation:
Tigre
Technical designation:
EC665
Version, Variant:
HAP
Type:
Conventional
Currently produced:
Y
Typical missions:
Military Combat Attack
Flight conditions:
IFR
First flight:
1991
Landing system:
wheels
Blades number:
4
Tail blades number:
3
weight
Weight class:
4
MTOW with external loads:
6100 kg13451 lbs
MTOW with only internal loading:
0 kg0 lbs
Empty weight:
4200 kg9261 lbs
External payload:
1800 kg3969 lbs
Internal payload:
0 kg0 lbs
Standard fuel tank:
1105 kg2437 lbs
with optionnal external fuel tank:
1689 kg3724 lbs
performance
Cruise speed:
230 km/h124 kt
Maximum cruise speed:
278 km/h150 kt
Vne:
322 km/h174 kt
Max negative g @ MTOW:
0 g
Max positive g @ MTOW:
0 g
Range with normal tanks:
800 km432 nm
Max range with auxiliary external tanks:
1280 km691 nm
Max endurance @ min consumption speed:
03:25:00 h:min
Rate of climb @ SL:
11.5 m/s2263 ft/min
Rate of climb @ SL @MTOW:
0 m/s0 ft/min
IGE max hovering altitude, MTOW:
0 m0 ft
IGE max hovering altitude, empty:
0 m0 ft
IGE max hovering altitude, ISA+20°C, MTOW:
0 m0 ft
IGE max hovering altitude, ISA+20°C, empty:
0 m0 ft
OGE max hovering altitude, MTOW:
3500 m11480 ft
OGE max hovering altitude, empty:
0 m0 ft
OGE max hovering altitude, ISA+20°C, MTOW:
0 m0 ft
OGE max hovering altitude, ISA+20°C, empty:
0 m0 ft
Service ceiling ISA, MTOW:
4000 m13120 ft
Max operating altitude, empty weight:
0 m0 ft
Highest use Temperature:
35 °C63 °F
Lowest use Temperature:
-30 °C-54 °F
power
APU in HC:

Engine manufacturer:
Turbomeca
Model:
MTR 390
Engines quantity:
2
Powerplant category:
turbine
Main rotor rotation speed:
0 rpm
Fuel consumption @ SL @ max continuous speed:
0 kg/kW/h0 lbs/hp/h
Minimum consumption speed @ SL:
0 km/h0 kt
Fuel consumption @ eco cruise speed @SL:
0 kg/h0 lbs/h
Fuel consumption @ min consumption speed @ SL:
0 kg/h0 lbs/h
Engines nominal power:
1746 kW2373 hp
Transmission shaft max continuous power:
0 kW0 hp
Transmission shaft max power:
0 kW0 hp
Takeoff power 5 min:
1936 kW2631 hp
OEI 30s power:
1160 kW1576 hp
OEI 2min power:
0 kW0 hp
OEI max continuous power :
0 kW0 hp
OEI max continuous transmission power:
0 kW0 hp
OEI 30 sec transmission power:
0 kW0 hp
OEI 2 min transmission power:
0 kW0 hp
dimensions
Overall length:
15.82 m52 ft
Rotor diameter:
13 m43 ft
Tail rotor diameter:
2.7 m9 ft
Fuselage length:
14.27 m47 ft
Overall height:
4.32 m14 ft
Main rotor blades chord:
0 m0 ft
Tail rotor blades chord:
0 m0 ft
Mast tilt angle:
0 °
noise
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
seating
Crew:
2
Max pax number:
0
use
Average price:
3.2e+07 $


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Label:
Booking.com
 
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