Basic Information

Category Helicopter Type Utility
Year Commissioned 2016 Year Decommissioned 0
Agility 1 Damage Points (DP) 3
Empty Weight 1925 kg Max Weight 3175 kg
Runway Information 0m (VTOL) TOD/LAD Physical Size Small Aircraft (0-12m)
Cost 0 Hypothetical No
Payload Weight 1250 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 FLIR Infrared, Surveillance Camera 0.00 - 30.00 nm 10 sec Infrared, 2nd Generation Imaging (1980s/1990s, LANTIRN, Litening) )

Sensor Coverage Diagram
Model Detection Angle Omnidirectional
Generic FLIR SB1, SB2, SMF1, SMF2, SMA1, SMA2, PB1, PB2, PMF1, PMF2, PMA1, PMA2

Weapon Loadouts Click to Expand Beta

Loadout Type Role Ready Time Combat Radius
Passenger   x 6
Trooper   x 4

Signatures

Type Front Side Rear
Visual Detection Range 2.56 nm 7 nm 2.56 nm
Visual Classification Range 1.24 nm 3.31 nm 1.88 nm
Infrared Detection Range 1.71 nm 6.6 nm 10.56 nm
Infrared Classification Range 1.03 nm 2.76 nm 1.03 nm
Radar, A-D Band (30-2000 MHz) -0.1 dBsm (0.9772 m²) 2.5 dBsm (1.78 m²) -0.1 dBsm (0.9772 m²)
Radar, E-M Band (2-100 GHz) -0.1 dBsm (0.9772 m²) 2.5 dBsm (1.78 m²) -0.1 dBsm (0.9772 m²)

Default Configuration

Model Comments

Datalink

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

Engines

Model Type Engine Count Military Thrust Afterburner Thrust Military Fuel Rate (SFC) Afterburner Fuel Rate (SFC) Hypothetical Comments
2x PW207D1 Helo Turboshaft 2 732 - 0.542 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 485