Mi-28 HAVOC
Crew |
2 |
Propulsion |
2 Turboshaft Engines |
|
Engine Model |
Klimov TW3-117VMA-SB3 / TV3-117VMA-SB3 |
|
Engine Power (each) |
1638 kW |
2197 shp |
Speed |
306 km/h |
165 kts |
Service Ceiling |
5.700 m |
18.701 ft |
Range |
450 km |
243 NM |
Empty Weight |
8.590 kg |
18.938 lbs |
max. Takeoff Weight |
11.700 kg |
25.794 lbs |
Rotor Blades
(main/tail) |
5/4 |
|
Main Rotor Diameter |
17,20 m |
56 ft 5 in |
Tail Rotor Diameter |
3,84 m |
12 ft 7 in |
Rotor Disc Area |
232,4 m² |
2502 ft² |
Length |
17,01 m |
55 ft 10 in |
Height |
3,82 m |
12 ft 6 in |
First Flight |
10.11.1982 |
Production Status |
in production |
ICAO Code |
MI28 |
NATO Code |
Havoc |
Data for (Version) |
Mil Mi-28NE |
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