1. Poland
  2. Aircraft
  3. W-3W/WA Sokol

Basic Information

Category Helicopter Type Attack
Year Commissioned 1990 Year Decommissioned 0
Agility 1 Damage Points (DP) 5
Empty Weight 3850 kg Max Weight 6400 kg
Runway Information 0m (VTOL) TOD/LAD Physical Size Medium Aircraft (12.1-18m)
Cost 0 Hypothetical No
Payload Weight 2550 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
Generic TV Camera Visual, Weapon Director TV Camera 0.00 - 80.00 nm 10 sec Visual, 2nd Generation TV Camera (1980s/1990s, AXX-1 TCS)

Sensor Coverage Diagram
Model Detection Angle Omnidirectional
Generic TV Camera SB1, SB2, SMF1, SMF2, SMA1, SMA2, PB1, PB2, PMF1, PMF2, PMA1, PMA2 否

Weapon Loadouts Click to Expand Beta

Loadout Type Role Ready Time Combat Radius
57mm Rocket   x 36
57mm Rocket   x 72

Signatures

Type Front Side Rear
Visual Detection Range 2.01 nm 5.53 nm 2.01 nm
Visual Classification Range 1.18 nm 3.18 nm 1.84 nm
Infrared Detection Range 2.01 nm 7.39 nm 11.25 nm
Infrared Classification Range 1.18 nm 3.18 nm 1.18 nm
Radar, A-D Band (30-2000 MHz) 1.9 dBsm (1.55 m²) 4.4 dBsm (2.75 m²) 1.9 dBsm (1.55 m²)
Radar, E-M Band (2-100 GHz) 1.9 dBsm (1.55 m²) 4.4 dBsm (2.75 m²) 1.9 dBsm (1.55 m²)

Default Configuration

Model Comments
23mm Gsh-23L [450 rnds] Helicopter, Mi-24VP

Datalink

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

Engines

Model Type Engine Count Military Thrust Afterburner Thrust Military Fuel Rate (SFC) Afterburner Fuel Rate (SFC) Hypothetical Comments
2x PZL-10B Helo Turboshaft 2 900 - 0.6 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 1375