A variant of the Mil Mi-34, certified by the Interstate Aviation Committee Aviation Register.  The Russian light training-multipurpose helicopter is capable of all aerobatic maneuvers.

Overview

Data on design, manufacture and status

Design authority: MVZ Mil

Primary manufacturer: MVZ Mil

Parent type: No type defined

Aircraft status: Operational

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift configuration: Single main rotor

Dedicated control device: Tail rotor

Crew required: 1-2

Crew seating: Side-by-side

Landing gear: Skids

Layout and Dimensions

Data on aircraft size

Overall Dimensions
Overall Height: 2.75 m 9.0 ft
Overall Length: 11.42 m 37.5 ft
Overall Width: 10.00 m 32.8 ft
Airframe Dimensions
Airframe Length: 8.75 m 28.7 ft
Airframe Width: 1.40 m 4.6 ft
Airframe Height: 2.45 m 8.0 ft
Landing Gear Dimensions
Landing Gear Base:  
Landing Gear Track: 2.24 m 7.3 ft
Cabin Dimensions
Cabin Internal Height:  
Cabin Internal Length:  
Cabin Internal Width:  

Weights and Performance

Data on aircraft weight and flight characteristics

Weights
Max Gross Weight (ground): 1,350 kg 2,976 lb
Max Gross Weight (airborne):  
Max Take-off Weight: 1,350 kg 2,976 lb
Empty Weight: 950 kg 2,094 lb
Useful Load: 400 kg 882 lb
Empty Weight Fraction: 0.704
Climb Performance
Max Rate of Climb:  
Hover Performance
Hover Ceiling IGE:  
Hover Ceiling OGE:  
Limitations
Max Level Flight Speed: 225 km/h 121 kts
Never Exceed Speed:  
Service Ceiling: 5,000 m 16,404 ft
Range and Endurance
Max Range: 420 km 227 nm
Max Endurance: 2 hrs 2 hrs

Engine Details

Aircraft powerplant (lift and/or propulsion)

Provided powerplant data is for uninstalled, sea level, static operations.

Powerplant
Number of engines: 1
Designation: Vedeneyev M-14V26 reciprocating
Manufacturer: Vedeneyev
Normal Ratings
Max continuous:  
Take-off / rated: 242 kW 325 hp
Intermediate:  
Maximum:  
OEI Ratings
OEI contingency:  
OEI continuous:  
OEI 30-second:  
OEI intermediate:  

Primary Lift Device

Data on primary lift devices such as main rotors

Main Rotor Characteristics
Diameter: 10.00 m 32.81 ft
RPM:  
Direction of Rotation: Clockwise
Hub Type: Semi-articulated
Main Rotor Blade Characteristics
Blade Construction: glass-fiber reinforced plastic (GFRP)
Blade Chord: 0.220 m 0.72 ft
Blade Tip Geometry: Flat
Blade Twist:  
Number of Blades: 4
Main Rotor Derived Characteristics
Disc Area: 78.54 m² 845.4 ft²
Disc Loading: 17.19 kg/m² 3.521 lb/ft²
Solidity: 0.0560
Main Rotor Blade Derived Characteristics
Blade area per blade: 1.10 m² 11.8 ft²
Tip Speed:  

Primary Control Device

Data on primary control devices such as tail rotors

Tail Rotor Characteristics
Diameter: 1.48 m 4.86 ft
Configuration: Pusher
Direction of Rotation: Top blade aft
RPM:  
Tail Rotor Blade Characteristics
Number of Blades: 2
Blade Construction: glass-fiber reinforced plastic (GFRP)
Blade Chord: 0.160 m 0.52 ft
Blade Twist:  
Tail Rotor Derived Characteristics
Disc Area: 1.72 m² 18.5 ft²
Solidity: 0.1376
Tail Rotor Blade Derived Characteristics
Tip Speed:  
Blade Area (per blade): 0.118 m² 1.27 ft²

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Resources related to the Mi-34S , provided by public sources across the internet.

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