Overview
In the late Cold War years, when Soviet engineers were focused on heavy transports and gunships, the Mil Mi-34 “Hermit” emerged as something different — a light, nimble helicopter designed for training, patrol, and civil use. Compact yet capable, it became the Soviet answer to the Western light helicopter market.
Specifications
Units
- Engine
- —
- Engine type
- -
- Power
- 320 hp · 239 kW
- Avionics
- —
- Wing tips
- No winglets
- Seats
- 3
- Crew
- —
- Cabin width
- —
- Cabin height
- —
- Cabin length
- —
- Exterior length
- 37 ft 6 in · 11.42 m
- Tail height
- —
- Fuselage diameter
- —
- Wing span
- 32 ft 10 in · 10.01 m
- Baggage volume
- 35 ft³ · 1.0 m³
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 3,000 lb · 1,350 kg
- Max landing weight
- —
- Max payload
- 1,200 lb · 550 kg
- Fuel capacity
- 50 gal · 200 L · 100 kg (Jet A)
- Max cruise speed
- 92 kt · 106 mph · 170 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- —
- Range
- 243 nm · 280 mi · 450 km
- Fuel burn
- 6.02 nm/gal · 2.94 km/L
- Ceiling
- 14,760 ft · 4,500 m
- Rate of climb
- 1,804 ft/min · 9 m/s
- Takeoff distance
- —
- Landing distance
- —
Gallery
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