The diameter of the main rotor, m |
32.00 |
The diameterof the tail rotor, m |
7.61 |
Length, m |
33.73 |
Height, m |
8.15 |
Weight, Kg |
|
empty |
28200 |
normal takeoff |
49600 |
maximum takeoff |
56000 |
Fuel tank, Lt |
12000 |
Engine type |
2 ГТД ЗМКБ Прогресс Д-136 |
Power, kW |
2 х 8380 |
Maximum speed, km/h |
295 |
Cruising speed, km/h |
255 |
The practical range, km |
2000 |
Service ceiling, m |
800 |
Static ceiling, m |
6500 |
Static ceiling, m |
1800 |
The crew, pers |
5 |
Coast: 8 000 000 USD
Mr. Vincent Vandendriessche
Mobile number: +32 485 20 37 39
phoenix.aviation.vdd@gmail.com
Mi-26 Technical Data
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