Catalog 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.