Basic Information

Category Helicopter Type Transport
Year Commissioned 2030 Year Decommissioned 0
Agility 2 Damage Points (DP) 5
Empty Weight 14000 kg Max Weight 16500 kg
Runway Information 0m (VTOL) TOD/LAD Physical Size Medium Aircraft (12.1-18m)
Cost 0 Hypothetical Yes
Payload Weight 0 kg Crew 4 people

Aircraft Capabilities

Nap-of-the-Earth (NOE) Fly-by-Wire Night Navigation (Ferry, Air-to-Air, Air-to-Surface Missiles) IRSS - Peak Temp Reduction (Cool-Air Mix)

Sensor Parameters

Model Purpose Range Scan Interval Generation
AN/APR-39D(V)2 RWR, Radar Warning Receiver 0.00 - 120.00 nm 5 sec Early 2010s

Sensor Coverage Diagram
Model Detection Angle Omnidirectional
AN/APR-39D(V)2 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
Trooper   x 12

Signatures

Type Front Side Rear
Visual Detection Range 2.95 nm 6.27 nm 2.95 nm
Visual Classification Range 1.51 nm 3.28 nm 2.55 nm
Infrared Detection Range 2.95 nm 6.98 nm 11.02 nm
Infrared Classification Range 1.6 nm 3.47 nm 1.6 nm
Radar, A-D Band (30-2000 MHz) 7.7 dBsm (5.89 m²) 10 dBsm (10.00 m²) 7.7 dBsm (5.89 m²)
Radar, E-M Band (2-100 GHz) 7.6 dBsm (5.75 m²) 9.8 dBsm (9.55 m²) 7.6 dBsm (5.75 m²)

Default Configuration

Model Comments
AN/ALE-47 CMDS x 4 [120 Cartridges] USN, Single Spectral, Chaff & Flare Dispenser
7.62mm M60D MG [400 rnds] Helicopter
7.62mm M60D MG [400 rnds] Helicopter

Datalink

Type Model Range Channels
Radio HF Radio [Secure] 300 nm 10

Engines

Model Type Engine Count Military Thrust Afterburner Thrust Military Fuel Rate (SFC) Afterburner Fuel Rate (SFC) Hypothetical Comments
1x Future Affordable Turbine Engine Helo Turboshaft 1 5000 - 0.5 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 1095