1. Soviet Union [-1991]
  2. Aircraft
  3. An-22 Cock

Basic Information

Category Fixed Wing Type Transport
Year Commissioned 1969 Year Decommissioned 1991
Agility 1 Damage Points (DP) 20
Empty Weight 118727 kg Max Weight 225000 kg
Runway Information 901-1400m TOD/LAD Physical Size Very Large Aircraft (26.1-75m)
Cost 0 Hypothetical No
Payload Weight 60000 kg Crew 7 people

Aircraft Capabilities

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

Sensor Parameters

Model Purpose Range Scan Interval Generation
Toad Stool [RBP-2] Radar, Weather and Navigation 0.20 - 35.00 nm 2 sec Early 1960s

Sensor Coverage Diagram
Model Detection Angle Omnidirectional
Toad Stool [RBP-2] SB1, SB2, SMF1, PB1, PB2, PMF2 否

Weapon Loadouts Click to Expand Beta

Loadout Type Role Ready Time Combat Radius
Paratrooper   x 151
Trooper   x 292

Signatures

Type Front Side Rear
Visual Detection Range 10.65 nm 17.69 nm 10.65 nm
Visual Classification Range 4.75 nm 8.38 nm 9.76 nm
Infrared Detection Range 10.65 nm 16.05 nm 21.51 nm
Infrared Classification Range 4.75 nm 8.38 nm 4.75 nm
Radar, A-D Band (30-2000 MHz) 22 dBsm (158.49 m²) 23.7 dBsm (234.42 m²) 22 dBsm (158.49 m²)
Radar, E-M Band (2-100 GHz) 22 dBsm (158.49 m²) 23.7 dBsm (234.42 m²) 22 dBsm (158.49 m²)

Default Configuration

Model Comments

Datalink

Type Model Range Channels
Radio UHF/VHF Radio [Unsecure] 100 nm 0
Radio 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 NK-12MA Turboprop 4 14795 - 0.36 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 96000