Mil Mi-38 (Prototype OP-4)
OP-4 was the fourth protoype in the development program for the Russian Mi-38 medium multipurpose helicopter.
Data is based on the year 2017 data points of the fourth protoype and 2000 Russia's Helicopter World catalog data points of the Mi-38.
Configuration
Primary flight and mechanical characteristicsVTOL type: Helicopter
Lift configuration: Single main rotor
Dedicated control device: Tail rotor
Crew required: 1-3
Crew seating: Side-by-side
Landing gear: Wheels (non-retractable)
Overall Dimensions
Data on aircraft sizeOverall Width: 21.10 m (69.2 ft)
Engine Details
Aircraft powerplant (lift and/or propulsion)Total number of engines: 2
Engine designation: Klimov TV7-117V turbine
Engine manufacturer: JSC Klimov United Engine Corporation
Take-off / rated power: 2088 kW (2799 hp)
Weights and Performance
Data on aircraft weight and flight characteristicsMax Gross Weight (ground): 15600 kg (34392 lb)
