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.
