Basic Information

Category Helicopter Type Transport
Year Commissioned 2005 Year Decommissioned 2032
Agility 1 Damage Points (DP) 5
Empty Weight 2720 kg Max Weight 4763 kg
Runway Information 0m (VTOL) TOD/LAD Physical Size Medium Aircraft (12.1-18m)
Cost 0 Hypothetical No
Payload Weight 2038 kg Crew 4 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-36 Star Safire II 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
AN/AAQ-36 Star Safire II SB1, SB2, SMF1, SMF2, SMA1, SMA2, SS1, SS2, PB1, PB2, PMF1, PMF2, PMA1, PMA2, PS1, PS2

Weapon Loadouts Click to Expand Beta

Loadout Type Role Ready Time Combat Radius

Signatures

Type Front Side Rear
Visual Detection Range 1.64 nm 4.89 nm 1.64 nm
Visual Classification Range 0.85 nm 2.44 nm 1.28 nm
Infrared Detection Range 1.64 nm 6.81 nm 10.39 nm
Infrared Classification Range 1 nm 2.87 nm 1 nm
Radar, A-D Band (30-2000 MHz) -0.6 dBsm (0.8710 m²) 2 dBsm (1.58 m²) -0.6 dBsm (0.8710 m²)
Radar, E-M Band (2-100 GHz) -0.6 dBsm (0.8710 m²) 2 dBsm (1.58 m²) -0.6 dBsm (0.8710 m²)

Default Configuration

Model Comments
7.62mm GAU-2 Minigun [900 rnds] Helicopter
12.7mm/50 MG [700 rnds] Helicopter, No Anti-Air Capability

Datalink

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

Engines

Model Type Engine Count Military Thrust Afterburner Thrust Military Fuel Rate (SFC) Afterburner Fuel Rate (SFC) Hypothetical Comments
1x T400-CP-400 Turbo Twin Pac Helo Turboshaft 1 1530 - 0.606 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 655