Mil Mi-28
Designated Havoc by NATO.
Configuration
Primary flight and mechanical characteristicsVTOL type: Helicopter
Lift configuration: Single main rotor
Dedicated control device: Tail rotor
Crew required: 2
Crew seating: Tandem
Landing gear: Wheels (non-retractable)
Layout and Dimensions
Data on aircraft size| Overall Dimensions | ||
|---|---|---|
| Overall Height: | 3.83 m | 12.6 ft |
| Overall Length: | 16.98 m | 55.7 ft |
| Overall Width: | 17.20 m | 56.4 ft |
| Airframe Dimensions | ||
|---|---|---|
| Airframe Length: | ||
| Airframe Width: | 5.50 m | 18.0 ft |
| 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 characteristicsCruise Speed: 270 km/h
| Weights | ||
|---|---|---|
| Max Gross Weight (ground): | 11,500 kg | 25,353 lb |
| Max Gross Weight (airborne): | ||
| Max Take-off Weight: | 11,500 kg | 25,353 lb |
| Empty Weight: | 8,095 kg | 17,846 lb |
| Useful Load: | 3,405 kg | 7,507 lb |
| Empty Weight Fraction: | 0.704 | |
| Climb Performance | ||
|---|---|---|
| Max Rate of Climb: | 14 m/s | 2,677 fpm |
| Hover Performance | ||
|---|---|---|
| Hover Ceiling IGE: | ||
| Hover Ceiling OGE: | 3,470 m | 11,385 ft |
| Limitations | ||
|---|---|---|
| Max Level Flight Speed: | 300 km/h | 162 kts |
| Never Exceed Speed: | ||
| Service Ceiling: | 5,700 m | 18,701 ft |
| Range and Endurance | ||
|---|---|---|
| Max Range: | 435 km | 235 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: | 2 | |
| Designation: | Motor Sich TV3-117VMA turbine | |
| Manufacturer: | Motor Sich | |
| Normal Ratings | ||
|---|---|---|
| Max continuous: | ||
| Take-off / rated: | 1640 kW | 2198 hp |
| Intermediate: | 1618 kW | 2169 hp |
| Maximum: | ||
| OEI Ratings | ||
|---|---|---|
| OEI contingency: | 1765 kW | 2366 hp |
| OEI continuous: | ||
| OEI 30-second: | ||
| OEI intermediate: | 1618 kW | 2169 hp |
Primary Lift Device
Data on primary lift devices such as main rotors| Main Rotor Characteristics | ||
|---|---|---|
| Diameter: | 17.20 m | 56.43 ft |
| RPM: | ||
| Direction of Rotation: | Clockwise | |
| Hub Type: | ||
| Main Rotor Blade Characteristics | ||
|---|---|---|
| Blade Construction: | ||
| Blade Chord: | ||
| Blade Tip Geometry: | Swept | |
| Blade Twist: | ||
| Number of Blades: | 5 | |
| Main Rotor Derived Characteristics | ||
|---|---|---|
| Disc Area: | 232.35 m² | 2501.1 ft² |
| Disc Loading: | 49.49 kg/m² | 10.137 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 fwd | |
| RPM: | ||
| Tail Rotor Blade Characteristics | ||
|---|---|---|
| Number of Blades: | 4 | |
| Blade Construction: | Asymmetrical X-shape | |
| 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-28 , provided by the Vertical Flight Society.Forum Proceedings
Vertiflite articles
Enter a search term in the box above.
Web files from vtol.org
Enter a search term in the box above.
Webpages from vtol.org
Enter a search term in the box above.
Related Public Resources
Resources related to the Mi-28 , provided by public sources across the internet.Publicly-funded resources provided by the US Government
Enter a search term in the box above.
Enter a search term in the box above.
Enter a search term in the box above.
Enter a search term in the box above.
Enter a search term in the box above.
Public resources provided by select scholarly and academic sources
Enter a search term in the box above.
Enter a search term in the box above.
Enter a search term in the box above.
Enter a search term in the box above.
