Modification of the Mil Mi-1.  Can be fitted with external tanks. Maximum sling load is 500 kg.

Overview

Data on design, manufacture and status

Design authority: MVZ Mil

Primary manufacturer: MVZ Mil

Parent type: Mil Mi-1

Aircraft status: No longer flying

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift configuration: Single main rotor

Dedicated control device: Tail rotor

Crew required: 1

Crew seating: Single seater

Landing gear: Wheels (non-retractable)

Layout and Dimensions

Data on aircraft size

Overall Dimensions
Overall Height:  
Overall Length:  
Overall Width: 14.30 m 46.9 ft
Airframe Dimensions
Airframe Length:  
Airframe Width:  
Airframe Height:  
Landing Gear Dimensions
Landing Gear Base:  
Landing Gear Track:  
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): 2,550 kg 5,622 lb
Max Gross Weight (airborne):  
Max Take-off Weight: 2,550 kg 5,622 lb
Empty Weight: 1,900 kg 4,189 lb
Useful Load: 650 kg 1,433 lb
Empty Weight Fraction: 0.745
Climb Performance
Max Rate of Climb:  
Hover Performance
Hover Ceiling IGE: 3,450 m 11,319 ft
Hover Ceiling OGE: 1,200 m 3,937 ft
Limitations
Max Level Flight Speed: 190 km/h 103 kts
Never Exceed Speed:  
Service Ceiling: 4,000 m 13,123 ft
Range and Endurance
Max Range: 360 km 194 nm
Max Endurance:  

Engine Details

Aircraft powerplant (lift and/or propulsion)

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

Powerplant
Number of engines: 1
Designation: Ivchenko AI-26VF reciprocating
Manufacturer: Ivchenko
Normal Ratings
Max continuous:  
Take-off / rated: 459 kW 615 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: 14.30 m 46.92 ft
RPM:  
Direction of Rotation: Clockwise
Hub Type:
Main Rotor Blade Characteristics
Blade Construction:
Blade Chord:  
Blade Tip Geometry: Conventional
Blade Twist:  
Number of Blades: 3
Main Rotor Derived Characteristics
Disc Area: 160.61 m² 1728.8 ft²
Disc Loading: 15.88 kg/m² 3.252 lb/ft²
Solidity:  
Main Rotor Blade Derived Characteristics
Blade area per blade:  
Tip Speed:  

Primary Control Device

Data on primary control devices such as tail rotors

Tail Rotor Characteristics
Diameter:  
Configuration: Pusher
Direction of Rotation: Top blade aft
RPM:  
Tail Rotor Blade Characteristics
Number of Blades: 3
Blade Construction:  
Blade Chord:  
Blade Twist:  
Tail Rotor Derived Characteristics
Disc Area:  
Solidity:  
Tail Rotor Blade Derived Characteristics
Tip Speed:  
Blade Area (per blade):  

Related VFS Resources

Resources related to the Mi-1M , provided by the Vertical Flight Society.
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Related Public Resources

Resources related to the Mi-1M , provided by public sources across the internet.

Images