1. Mali [1960-]
  2. Aircraft
  3. Mi-171Sh Hip H

Basic Information

Category Helicopter Type Transport
Year Commissioned 2021 Year Decommissioned 0
Agility 1 Damage Points (DP) 10
Empty Weight 7160 kg Max Weight 12000 kg
Runway Information 0m (VTOL) TOD/LAD Physical Size Large Aircraft (18.1-26m)
Cost 0 Hypothetical No
Payload Weight 0 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 FLIR Infrared, Surveillance Camera 0.00 - 30.00 nm 10 sec Infrared, 2nd Generation Imaging (1980s/1990s, LANTIRN, Litening) )

Sensor Coverage Diagram
Model Detection Angle Omnidirectional
Generic FLIR 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
Trooper   x 12
57mm Rocket   x 108
Trooper   x 24

Signatures

Type Front Side Rear
Visual Detection Range 2.45 nm 6.69 nm 2.45 nm
Visual Classification Range 1.19 nm 3.17 nm 1.91 nm
Infrared Detection Range 2.45 nm 8.39 nm 12.15 nm
Infrared Classification Range 1.39 nm 3.73 nm 1.39 nm
Radar, A-D Band (30-2000 MHz) 4.3 dBsm (2.69 m²) 6.6 dBsm (4.57 m²) 4.3 dBsm (2.69 m²)
Radar, E-M Band (2-100 GHz) 4.3 dBsm (2.69 m²) 6.6 dBsm (4.57 m²) 4.3 dBsm (2.69 m²)

Default Configuration

Model Comments
7.62mm MG [400 rnds] Helicopter

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 TV3-117MT Helo Turboshaft 2 2225 - 0.23 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 1495