1. Libya
  2. Aircraft
  3. An-124 Condor

Basic Information

Category Fixed Wing Type Transport
Year Commissioned 1987 Year Decommissioned 2019
Agility 1 Damage Points (DP) 20
Empty Weight 177000 kg Max Weight 405000 kg
Runway Information 2601-3200m TOD/LAD Physical Size Very Large Aircraft (26.1-75m)
Cost 0 Hypothetical No
Payload Weight 120000 kg Crew 7 people

Aircraft Capabilities

Night Navigation (Ferry, Air-to-Air, Air-to-Surface Missiles) Probe Refueling

Sensor Parameters

Model Purpose Range Scan Interval Generation
Generic Weather Radar Radar, Weather 0.20 - 35.00 nm 2 sec Early 1970s

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

Weapon Loadouts Click to Expand Beta

Loadout Type Role Ready Time Combat Radius
No Data
No Data
No Data

Signatures

Type Front Side Rear
Visual Detection Range 18.32 nm 33.08 nm 18.32 nm
Visual Classification Range 6.38 nm 12.08 nm 13.43 nm
Infrared Detection Range 12.22 nm 18.59 nm 22.69 nm
Infrared Classification Range 5.32 nm 10.07 nm 5.32 nm
Radar, A-D Band (30-2000 MHz) 23.7 dBsm (234.42 m²) 25.2 dBsm (331.13 m²) 23.7 dBsm (234.42 m²)
Radar, E-M Band (2-100 GHz) 23.7 dBsm (234.42 m²) 25.2 dBsm (331.13 m²) 23.7 dBsm (234.42 m²)

Default Configuration

Model Comments
No Data

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
4x D-18T Turbofan 4 23453 - 0.345 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 213740