Helicopter Mi-34 Hermit
<-------------Dimensions --------------------------->
Diameter main Rotor = 10m
chord  = 0,22m
airfoil NACA 230
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Diameter tail Rotor = 1,48m
chord = 0,1m
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Length with rotated propellers = 11,48m
Length of a fuselage = 8,713m
Breadth of a fuselage = 1,42m
Altitude up to a rotor hub = 2,5m
Track of skis =2,06m
<---------- Mass ---------->
Mass empty = 1010 kg
Normal ascent = 1280 kg
Maximum ascent = 1350 kg
Intrinsic fuel = 120 kg
fuel = 160 liters on 2 hour
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The payload, kg is maximum:
In a fuselage =240
On the choronomic suspension =300
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Maximum permissible overload:
Positive 2,5G
Negative 0,5G
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<-- Power plant -->
Engine = M-14B26B x1 --Mi-34(and Ka-26)
Power = 325-370 hp
Engine = VAZ-426 x2 --Mi-34VAZ
Power = 270 hp
------------
Engine RPM = 2800
Main rotor RPM = 390
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At temperatures from -35 to +45
<-- Performance -->
Crew = 1-2
The passengers = 2-3
Cruising speed = 180 kmh
Maximum speed = 220 kmh
Maximum back speed = 130 kmh
Radius of action = 150 km
Distance of flying = 360 km
Static ceiling = 1500 m
Service ceiling = 4500 m
Rate of climb = 550 m/min
Duration = 2,1 hour
