Mi-24/35 Hind

4
Country: Czech
Operator: Czech Air Force
Total lenght: 19.79 m (otáčajúce sa rotory)
Main rotor diameter: 17.3 m
Height: 6.5 m
Maximum take-off weight: 12.500 kg
Ceiling: 4.500 m
Range: 750 km
Maximum speed : 310 km/hod.

More details:

  • rate of climb:   750 m/min.
  • engine/power: 2 × TV3-117VMA, 1,600 kW (2,200 hp) each

Source: http://www.acr.army.cz

https://en.wikipedia.org/wiki/Mil_Mi-24#Specifications

Photo (Source:  http://www.acr.army.cz)

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