1. Japan
  2. Aircraft
  3. AW.139

Basic Information

Category Helicopter Type Utility
Year Commissioned 2006 Year Decommissioned 0
Agility 1 Damage Points (DP) 3
Empty Weight 3622 kg Max Weight 6400 kg
Runway Information 0m (VTOL) TOD/LAD Physical Size Small Aircraft (0-12m)
Cost 0 Hypothetical No
Payload Weight 0 kg Crew 2 people

Aircraft Capabilities

Nap-of-the-Earth (NOE) Night Navigation (Ferry, Air-to-Air, Air-to-Surface Missiles)

Sensor Parameters

Model Purpose Range Scan Interval Generation
Generic IR Camera Infrared, Surveillance Camera 0.00 - 30.00 nm 10 sec Infrared, 3rd Generation Imaging (2000s/2010s, Impr LANTIRN, Litening II/III, ATFLIR)

Sensor Coverage Diagram
Model Detection Angle Omnidirectional
Generic IR Camera SB1, SB2, SMF1, SMF2, SMA1, SMA2, SS1, SS2, PB1, PB2, PMF1, PMF2, PMA1, PMA2, PS1, PS2 是

Weapon Loadouts Click to Expand Beta

Loadout Type Role Ready Time Combat Radius
Trooper   x 12
Trooper   x 12

Signatures

Type Front Side Rear
Visual Detection Range 3.09 nm 9.18 nm 3.09 nm
Visual Classification Range 1.45 nm 4.15 nm 2.26 nm
Infrared Detection Range 2.06 nm 7.91 nm 11.35 nm
Infrared Classification Range 1.21 nm 3.46 nm 1.21 nm
Radar, A-D Band (30-2000 MHz) 2.2 dBsm (1.66 m²) 4.6 dBsm (2.88 m²) 2.2 dBsm (1.66 m²)
Radar, E-M Band (2-100 GHz) 2.2 dBsm (1.66 m²) 4.6 dBsm (2.88 m²) 2.2 dBsm (1.66 m²)

Default Configuration

Model Comments

Datalink

Type Model Range Channels
Radio UHF/VHF Radio [Unsecure] 100 nm 0
Radio HF Radio [Unsecure] 300 nm 10

Engines

Model Type Engine Count Military Thrust Afterburner Thrust Military Fuel Rate (SFC) Afterburner Fuel Rate (SFC) Hypothetical Comments
2x PT6C-67C Helo Turboshaft 2 1531 - 0.5 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 785