1. Sri Lanka
  2. Aircraft
  3. K-8W Karakorum

Basic Information

Category Fixed Wing Type Trainer
Year Commissioned 2001 Year Decommissioned 0
Agility 3 Damage Points (DP) 3
Empty Weight 2687 kg Max Weight 4330 kg
Runway Information 451-900m TOD/LAD Physical Size Small Aircraft (0-12m)
Cost 0 Hypothetical No
Payload Weight 950 kg Crew 2 people

Aircraft Capabilities

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

Signatures

Type Front Side Rear
Visual Detection Range 2.2 nm 4.61 nm 2.2 nm
Visual Classification Range 1.27 nm 2.73 nm 2.02 nm
Infrared Detection Range 2.2 nm 6.55 nm 11.65 nm
Infrared Classification Range 1.27 nm 2.73 nm 1.27 nm
Radar, A-D Band (30-2000 MHz) 3 dBsm (2.00 m²) 5.4 dBsm (3.47 m²) 3 dBsm (2.00 m²)
Radar, E-M Band (2-100 GHz) 3 dBsm (2.00 m²) 5.4 dBsm (3.47 m²) 3 dBsm (2.00 m²)

Default Configuration

Model Comments

Datalink

Type Model Range Channels
Radio UHF/VHF Radio [Unsecure] 100 nm 0
Radio HF Radio [Unsecure] 300 nm 10

Engines

Model Type Engine Count Military Thrust Afterburner Thrust Military Fuel Rate (SFC) Afterburner Fuel Rate (SFC) Hypothetical Comments
1x TFE-731-2A-2A Turbojet 1 1635 - 0.504 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 780