1. Vietnam [1975-]
  2. Aircraft
  3. Mi-24A Hind A

Basic Information

Category Helicopter Type Attack
Year Commissioned 1980 Year Decommissioned 1994
Agility 2 Damage Points (DP) 5
Empty Weight 8200 kg Max Weight 11500 kg
Runway Information 0m (VTOL) TOD/LAD Physical Size Medium Aircraft (12.1-18m)
Cost 0 Hypothetical No
Payload Weight 1480 kg Crew 3 people

Aircraft Capabilities

Nap-of-the-Earth (NOE) Night Navigation (Ferry, Air-to-Air, Air-to-Surface Missiles) Bombsight - Ballistic Computing IRSS - Peak Temp Reduction (Cool-Air Mix)

Sensor Parameters

Model Purpose Range Scan Interval Generation
No Data

Sensor Coverage Diagram
Model Detection Angle Omnidirectional
No Data

Weapon Loadouts Click to Expand Beta

Loadout Type Role Ready Time Combat Radius
No Data
No Data

Signatures

Type Front Side Rear
Visual Detection Range 2.01 nm 6.19 nm 2.01 nm
Visual Classification Range 1.18 nm 3.49 nm 1.84 nm
Infrared Detection Range 2.01 nm 7.16 nm 10.12 nm
Infrared Classification Range 1.18 nm 3.49 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
12.7mm A-12.7 [200 rnds] Helicopter, Mi-24A

Datalink

Type Model Range Channels
Radio UHF/VHF Radio [Unsecure] 100 nm 0
Radio AT-2/6/8/9 Guidance Unit 10 nm 1

Engines

Model Type Engine Count Military Thrust Afterburner Thrust Military Fuel Rate (SFC) Afterburner Fuel Rate (SFC) Hypothetical Comments
2x TV3-117V Helo Turboshaft 2 2200 - 0.23 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 1500