Variant of the Mil Mi-24.  The helicopter was presented in Le Bourget at the Moscow Air Show '95; the design includes alternate controls for the gunner in the event the pilot is wounded.  Maximum internal and external payload are 1500 kg and 2400 kg, respectively.  Ammunition loading is 2860 kg.


Data on design, manufacture and status

Design authority: MVZ Mil

Primary manufacturer: MVZ Mil

Parent type: Mil Mi-24

Aircraft status: Status unknown


Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift configuration: Single main rotor

Dedicated control device: Tail rotor

Crew required: 2

Crew seating: Tandem

Landing gear: Wheels (non-retractable)

Layout and Dimensions

Data on aircraft size

Overall Dimensions
Overall Height:  
Overall Length:  
Overall Width:  
Airframe Dimensions
Airframe Length: 17.50 m 57.4 ft
Airframe Width: 5.27 m 17.3 ft
Airframe Height: 3.97 m 13.0 ft
Landing Gear Dimensions
Landing Gear Base:  
Landing Gear Track:  
Cabin Dimensions
Cabin Internal Height: 1.45 m 4.8 ft
Cabin Internal Length: 2.50 m 8.2 ft
Cabin Internal Width: 1.20 m 3.9 ft

Weights and Performance

Data on aircraft weight and flight characteristics

Cruise Speed: 260 km/h

Max Gross Weight (ground): 11,500 kg 25,353 lb
Max Gross Weight (airborne):  
Max Take-off Weight: 11,500 kg 25,353 lb
Empty Weight: 8,050 kg 17,747 lb
Useful Load: 3,450 kg 7,606 lb
Empty Weight Fraction: 0.700
Climb Performance
Max Rate of Climb: 12 m/s 2,441 fpm
Hover Performance
Hover Ceiling IGE:  
Hover Ceiling OGE: 2,100 m 6,890 ft
Max Level Flight Speed: 312 km/h 168 kts
Never Exceed Speed:  
Service Ceiling: 5,750 m 18,865 ft
Range and Endurance
Max Range: 415 km 224 nm
Max Endurance:  

Engine Details

Aircraft powerplant (lift and/or propulsion)

Provided powerplant data is for uninstalled, sea level, static operations.

Number of engines: 2
Designation: Motor Sich TV3-117VMA turbine
Manufacturer: Motor Sich
Normal Ratings
Max continuous:  
Take-off / rated: 1640 kW 2198 hp
Intermediate: 1618 kW 2169 hp
OEI Ratings
OEI contingency: 1765 kW 2366 hp
OEI continuous:  
OEI 30-second:  
OEI intermediate: 1618 kW 2169 hp

Primary Lift Device

Data on primary lift devices such as main rotors

Main Rotor Characteristics
Diameter: 17.20 m 56.43 ft
Direction of Rotation: Unknown
Hub Type:
Main Rotor Blade Characteristics
Blade Construction:
Blade Chord:  
Blade Tip Geometry:
Blade Twist:  
Number of Blades: 5
Main Rotor Derived Characteristics
Disc Area: 232.35 m² 2501.1 ft²
Disc Loading: 49.49 kg/m² 10.137 lb/ft²
Main Rotor Blade Derived Characteristics
Blade area per blade:  
Tip Speed:  

Primary Control Device

Data on primary control devices such as tail rotors

Tail Rotor Characteristics
Configuration: Unknown
Direction of Rotation: Unknown
Tail Rotor Blade Characteristics
Number of Blades: 4
Blade Construction: Asymmetrical X-shape
Blade Chord:  
Blade Twist:  
Tail Rotor Derived Characteristics
Disc Area:  
Tail Rotor Blade Derived Characteristics
Tip Speed:  
Blade Area (per blade):  

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