Variant of the Mi-8. Unlike the Mi-8T, the turboshaft engine is equipped with deflectors to prevent dust ingestion. The military-transport helicopter has an armored cabin and is eqipped with 7.62 mm machine guns. The Mi-8MTV family is capable of a higher hover ceiling than the Mi-8MT.
The aircraft is part of the Mil Mi-17 export series.
Design authority: MVZ Mil
Primary manufacturer: MVZ Mil
Parent type: Mil Mi-8/Mi-14/Mi-17
Aircraft status: Status unknown
VTOL type: Helicopter
Lift configuration: Single main rotor
Dedicated control device: Tail rotor
Crew required: 3
Crew seating: Side-by-side
Landing gear: Wheels (non-retractable)
Overall Dimensions | ||
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Overall Height: | 5.65 m | 18.5 ft |
Overall Length: | 25.24 m | 82.8 ft |
Overall Width: | 21.30 m | 69.9 ft |
Airframe Dimensions | ||
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Airframe Length: | 18.22 m | 59.8 ft |
Airframe Width: | 4.50 m | 14.8 ft |
Airframe Height: | 4.75 m | 15.6 ft |
Landing Gear Dimensions | ||
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Landing Gear Base: | 4.26 m | 14.0 ft |
Landing Gear Track: | 4.80 m | 15.7 ft |
Cabin Dimensions | ||
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Cabin Internal Height: | 1.80 m | 5.9 ft |
Cabin Internal Length: | 5.34 m | 17.5 ft |
Cabin Internal Width: | 2.34 m | 7.7 ft |
Normal Speed: 250 km/h; Cruise Speed: 240 km/h; Hover Ceiling (unspecified): 3980 m
Weights | ||
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Max Gross Weight (ground): | 12,000 kg | 26,455 lb |
Max Gross Weight (airborne): | ||
Max Take-off Weight: | 13,000 kg | 28,660 lb |
Empty Weight: | 7,369 kg | 16,246 lb |
Useful Load: | 5,631 kg | 12,414 lb |
Empty Weight Fraction: | 0.567 |
Climb Performance | ||
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Max Rate of Climb: |
Hover Performance | ||
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Hover Ceiling IGE: | ||
Hover Ceiling OGE: |
Limitations | ||
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Max Level Flight Speed: | ||
Never Exceed Speed: | ||
Service Ceiling: | 4,900 m | 16,076 ft |
Range and Endurance | ||
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Max Range: | 495 km | 267 nm |
Max Endurance: |
Provided powerplant data is for uninstalled, sea level, static operations.
Powerplant | ||
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Number of engines: | 2 | |
Designation: | Motor Sich TV3-117VMA turbine | |
Manufacturer: | Motor Sich |
Normal Ratings | ||
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Max continuous: | ||
Take-off / rated: | 1640 kW | 2198 hp |
Intermediate: | 1618 kW | 2169 hp |
Maximum: |
OEI Ratings | ||
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OEI contingency: | 1765 kW | 2366 hp |
OEI continuous: | ||
OEI 30-second: | ||
OEI intermediate: | 1618 kW | 2169 hp |
Main Rotor Characteristics | ||
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Diameter: | 21.30 m | 69.88 ft |
RPM: | ||
Direction of Rotation: | Clockwise | |
Hub Type: |
Main Rotor Blade Characteristics | ||
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Blade Construction: | All-metal | |
Blade Chord: | ||
Blade Tip Geometry: | Conventional | |
Blade Twist: | ||
Number of Blades: | 5 |
Main Rotor Derived Characteristics | ||
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Disc Area: | 356.33 m² | 3835.6 ft² |
Disc Loading: | 33.68 kg/m² | 6.898 lb/ft² |
Solidity: |
Main Rotor Blade Derived Characteristics | ||
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Blade area per blade: | ||
Tip Speed: |
Tail Rotor Characteristics | ||
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Diameter: | 3.91 m | 12.83 ft |
Configuration: | Pusher | |
Direction of Rotation: | Top blade fwd | |
RPM: |
Tail Rotor Blade Characteristics | ||
---|---|---|
Number of Blades: | 3 | |
Blade Construction: | ||
Blade Chord: | ||
Blade Twist: |
Tail Rotor Derived Characteristics | ||
---|---|---|
Disc Area: | 12.01 m² | 129.2 ft² |
Solidity: |
Tail Rotor Blade Derived Characteristics | ||
---|---|---|
Tip Speed: | ||
Blade Area (per blade): |