1. Argentina
  2. Aircraft
  3. A-109 Agusta

Basic Information

Category Helicopter Type Transport
Year Commissioned 1980 Year Decommissioned 2006
Agility 1 Damage Points (DP) 3
Empty Weight 1415 kg Max Weight 2450 kg
Runway Information 0m (VTOL) TOD/LAD Physical Size Small Aircraft (0-12m)
Cost 0 Hypothetical No
Payload Weight 1035 kg Crew 2 people

Aircraft Capabilities

Nap-of-the-Earth (NOE) Night Navigation (Ferry, Air-to-Air, Air-to-Surface Missiles) Bombsight - Ballistic Computing

Sensor Parameters

Model Purpose Range Scan Interval Generation

Sensor Coverage Diagram
Model Detection Angle Omnidirectional

Weapon Loadouts Click to Expand Beta

Loadout Type Role Ready Time Combat Radius
Trooper   x 4

Signatures

Type Front Side Rear
Visual Detection Range 1.51 nm 4.14 nm 1.51 nm
Visual Classification Range 0.93 nm 2.5 nm 1.39 nm
Infrared Detection Range 1.51 nm 6.09 nm 10.07 nm
Infrared Classification Range 0.93 nm 2.5 nm 0.93 nm
Radar, A-D Band (30-2000 MHz) -1.5 dBsm (0.7079 m²) 1.1 dBsm (1.29 m²) -1.5 dBsm (0.7079 m²)
Radar, E-M Band (2-100 GHz) -1.5 dBsm (0.7079 m²) 1.1 dBsm (1.29 m²) -1.5 dBsm (0.7079 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 250-C20R/1 Helo Turboshaft 2 450 - 0.608 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 485