Basic Information

Category Helicopter Type Transport
Year Commissioned 1990 Year Decommissioned 0
Agility 1 Damage Points (DP) 3
Empty Weight 720 kg Max Weight 1405 kg
Runway Information 0m (VTOL) TOD/LAD Physical Size Small Aircraft (0-12m)
Cost 0 Hypothetical No
Payload Weight 455 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
AN/AAQ-16 AESOP Infrared, Surveillance & Navigation Camera 0.00 - 15.00 nm 10 sec Infrared, 2nd Generation Imaging (1980s/1990s, LANTIRN, Litening) )

Sensor Coverage Diagram
Model Detection Angle Omnidirectional
AN/AAQ-16 AESOP 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
Ranger   x 4

Signatures

Type Front Side Rear
Visual Detection Range 0.91 nm 2.8 nm 0.91 nm
Visual Classification Range 0.57 nm 1.67 nm 0.78 nm
Infrared Detection Range 1.01 nm 5.04 nm 8.6 nm
Infrared Classification Range 0.66 nm 1.97 nm 0.66 nm
Radar, A-D Band (30-2000 MHz) -6.4 dBsm (0.2291 m²) -3.6 dBsm (0.4365 m²) -6.4 dBsm (0.2291 m²)
Radar, E-M Band (2-100 GHz) -6.4 dBsm (0.2291 m²) -3.6 dBsm (0.4365 m²) -6.4 dBsm (0.2291 m²)

Default Configuration

Model Comments

Datalink

Type Model Range Channels
Radio UHF/VHF Radio [Secure] 100 nm 0
Radio UHF/VHF Radio [Secure] 100 nm 0

Engines

Model Type Engine Count Military Thrust Afterburner Thrust Military Fuel Rate (SFC) Afterburner Fuel Rate (SFC) Hypothetical Comments
1x 250-C20B Helo Turboshaft 1 420 - 0.65 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 205