Specifications for the
Mil Mi-24 (Hind)
Armed Assault / Attack Helicopter
Focus Model: Mil Mi-24 (Hind)
Country of Origin: Soviet Union
Manufacturer: Mil Moscow Helicopter Plant - Soviet Union
Initial Year of Service: 1973
Crew: 3 + 8
Length: 57.41 ft (17.5 m)
Width: 21.29 ft (6.49 m)
Height: 13.02ft (3.97 m)
Weight (Empty): 18,078 lb (8,200 kg)
Weight (MTOW): 26,455 lb (12,000 kg)
Powerplant: 2 x Isotov TV3-117 Turboshaft engines driving a five-blade main rotor and a three-blade tail rotor.
Maximum Speed: 208 mph (335kmh; 181 kts)
Maximum Range: 99 miles (160km)
Service Ceiling: 14,747 ft (4,495 m; 2.8 miles)
Rate-of-Climb: 2,460 feet-per-minute (750 m/min)
Depending on Production Variant:
1 x 12.7mm heavy machine gun in fixed nose emplacement.
1 x 12.7mm Yakushev-Borzov four-barrel machine gun (Gatling arrangement) in powered chin turret.
1 x 23mm GSh-23L cannon (twin arrangement) in powered chin turret.
1 x 30mm GSh-30K cannon (twin arrangement) in fixed, starboard fuselage side emplacement.
Additional underwing stores can include (across six hardpoints):
Anti-Tank Guided Missiles
Rocket Pods (Various Rocket Counts and Calibers)
Machine Gun Pods
Munitions Dispenser Pods
Mine Dispenser Pods
Conventional Drop Bombs
V-24 (Hind) - Protype
Afghanistan; Algeria; Angola, Armenia, Azerbaijan; Belarus; Bulgaria; Chad; Cyprus; Croatia; Cuba; Czech Republic; East Germany; Equatorial Guinea; Eritrea; Ethiopia; Georgia; Guinea; Hungary; India; Indonesia; Iraq; Iran; Kazakhstan; Kyrgizia; Libya; Macedonia; Mozambique; Nicaragua; Nigeria; North Korea; Pakistan; Peru; Poland; Russia; Rwanda; Serbia; Sierra Leone; Slovakia; South Africa; Soviet Union; Sri Lanka; Sudan; Syria; Tajikistan; Ukraine; Uzbekistan; Venezuela; Vietnam; Yemen; Zimbabwe; United States