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Military


Mi-24 HIND
Mi-25 HIND D
Mi-35 HIND E

Specifications
Country of Origin Russia
Builder MIL
Date of Introduction 1976 (HIND D)
Role Assault, gunship, antitank
Similar Aircraft AH-1 Cobra (all models), UH-60 Black Hawk, AH-64 Apache, Mangusta A129
Blades Main rotor: 5
Tail rotor: 3
Rotor diameter Main Rotor : 17.3 meters
Tail Rotor: 3.9 meters
Wing span 6.5 meters
Length Length : 21.6 m (rotors turning)
Length : 17.5 m (fuselage)
Height 13 ft., 11 in.
6.5 meters (gear extended)
Cargo Compartment Dimensions Floor Length: 2.5 meters
Width: 1.5 meters
Height: 1.2 meters
Weight Maximum Gross: 11,500 kg
Normal Takeoff: 11,100 kg
Empty: 8,500 kg
Fuel Internal: 1,840 liters
Internal Aux Tank (in cabin): 1,227 liters
External Fuel Tank: 500 liters ea.
Fuel consumptionl 360 l/h (ground)
350 l/h (air)
Engine 2 x 2,200 shp Isotov TV-3-117 turbines
Maximum speed 168 mph / 335 km/h
Cruising speed 295 km/h
Range Normal Load: 450 km
With Aux Fuel: 950 km
Service Ceiling 4,500 meters
Hover out of ground effect: 1,500 meters
in ground effect : 2,200 meters
Vertical Climb Rate 15 m/s
Max "G" Force 1.75 g
Standard Payload Internal load: 8 combat troops or 4 litters
External weapons load: 1,500 kg
External load (no weapons): 2,500 kg
Armament 12.7-mm 4x Barrel Machinegun, YaKB-12.7:
Range (m): (practical) 1,500
Elevation/Traverse: 20 up to 60 down/ 120
Ammo Type: HEFI, APT, Duplex, DuplexT
Rate of Fire (rpm): up to 4,500 (pilot selectable) 30-mm Twin Barrel Cannon, GSh-30K:
Range (m): (practical) 4,000
Elevation/Traverse: None (rigidly mounted)
Ammo Type: HEFI, HEI, APT, APE, CC
Rate of Fire (rpm): 300, or 2,000 to 2,600
  • 750 - 1x twin 30-mm gun, or
  • 1,470 - 12.7-mm 4 barrel turret gun
  • 2-12 - AT-2C or AT-6C Spiral ATGMs
  • 2-4 - 80-mm S-8 rocket pods (20 ea.)
  • 2-4 - 57-mm S-5 rocket pods (32 ea.)
  • 940 - GSh-23L twin 23-mm MG pods
  • 4 - 250-kg bombs FAB-250
  • 2 - 500-kg bombs
  • 500 liters External fuel tanks Most Probable Armament
  • HIND D: Turret-mounted 4-barrel 12.7-mm Gatling type machinegun, 57-mm rockets, AT-2C/ SWATTER ATGMs.
  • HIND E: Turret-mounted 4-barrel 12.7-mm Gatling type machinegun or twin barrel 23-mm turret gun, 57-mm rockets, AT-6C/ SPIRAL ATGMs.
  • HIND F: Fixed 30-mm twin gun on the right fuselage side, 57-mm rockets, AT-6C/ SPIRAL ATGMs.
Loaded combat troops can fire personal weapons through cabin windows.
Sensors FLIR, RWR, laser designator
AVIONICS
  • The ATGM targeting system uses a low-level light TV, a laser designator, FLIR, air data sensor, and a missile guidance transmitter.
  • HIND D versions are primarily daytime aircraft only. Some HIND E and Mi-35 series export versions have upgraded night and weather capabilities, better avionics, weather radar, autopilot, HUD, GPS, NVG compatibility, more armor, and an increased weapons load provided by the French company Sextant Avionique.
Survivability
  • Main and tail rotors electrically deiced.
  • Infrared signature suppressors can be mounted on engine exhausts.
  • Radar warning receivers, IFF, Infrared jammer, rotor brake, chaff and flares.
  • Armored cockpit.
Crew Two (pilots in tandem cockpits)
Cost  
User Countries At least 34 countries -- Armenia, Afghanistan, Algeria, Angola, Belarus, Bulgaria, Cambodia, CIS, Cuba, Czech Republic, Ethiopia, Georgia, Germany, Hungary, Iran, Iraq, Libya, Mongolia, Mozambique, Nicaragua, North Korea, Peru, Poland, Slovakia, South Yemen, Syria, Ukraine, Vietnam



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