Basic Information

Category Helicopter Type Transport
Year Commissioned 1996 Year Decommissioned 0
Agility 1 Damage Points (DP) 5
Empty Weight 4330 kg Max Weight 8600 kg
Runway Information 0m (VTOL) TOD/LAD Physical Size Medium Aircraft (12.1-18m)
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 Navigation Radar Radar, Navigation 0.20 - 20.00 nm 2 sec Early 1970s

Sensor Coverage Diagram
Model Detection Angle Omnidirectional
Generic Navigation Radar SB1, SB2, SMF1, PB1, PB2, PMF2

Weapon Loadouts Click to Expand Beta

Loadout Type Role Ready Time Combat Radius

Signatures

Type Front Side Rear
Visual Detection Range 1.98 nm 5.8 nm 1.98 nm
Visual Classification Range 1.17 nm 3.31 nm 1.82 nm
Infrared Detection Range 1.98 nm 7.63 nm 11.19 nm
Infrared Classification Range 1.17 nm 3.31 nm 1.17 nm
Radar, A-D Band (30-2000 MHz) 1.7 dBsm (1.48 m²) 4.2 dBsm (2.63 m²) 1.7 dBsm (1.48 m²)
Radar, E-M Band (2-100 GHz) 1.7 dBsm (1.48 m²) 4.2 dBsm (2.63 m²) 1.7 dBsm (1.48 m²)

Default Configuration

Model Comments

Datalink

Type Model Range Channels
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
2x Makila 1A1 Helo Turboshaft 2 1877 - 0.481 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 1360