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  • Catalog Characteristics

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    Name

    Characteristics

    Dimensions

    Main rotor diameter:

    17.3 m

    Tail rotor diameter:

    3,908 m

    Height above ground together with rotors

    5.47 m

    Fuselage length:

    17.51 (17,23 for Mi-24VM) m

    Fuselage width:

    1.7 m

    Fuselage height:

    3.9 m

    Wingspan:

    6.4 m

    Basic weights

    Empty:

    7580 kg

    Normal take-off weight:

    10 500 kg

    Maximum take-off weight:

    Maximum airlift capacity:

    2400 kg

    Load weight on the sling:

    2400 kg

    Internal fuel capacity:

    2100 kg

    Fuel pod capacity:

    up to 3000 kg

    Power plant

    Quantity, type, grade:

    2 engines TV3-117V (BMA – altitude, upgraded engine – A series)

    Power:

    2 x 2500 HP

    Flight specifications

    Crew:

    2-3 people.

    Passengers:

    up to 8 paratroopers, 2 seriously wounded on stretchers and 2 lightly wounded and the medical worker.

    Cruising speed:

    270 km/h

    Maximum speed in horizontal flight:

    335 km/h

    Practical flight range:

    450 km

    Ferry flight range:

    1000 km

    Average fuel consumption:

    780 l/h

    Static ceiling:

    1400 m

    Dynamic ceiling:

    4950 m

    Maximum operational overload:

    −1,3/+3

    Allowable bank angle:

    50 degrees.

    Allowable pitch angle:

    30 degrees.

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