
History:
The Mi-17 helicopter was developed
at the Mil Design Bureau and is based on the Mi-8 helicopter.
While the Russian armed forces called it the Mi-8MT, the designation
Mi-17 is meant for export models. The Mi-17 can be recognized
because it has the tail rotor on the right side, instead of the
left side as seen on the Mi-8. The Mi-17 added a number of improvements
to its predecessor, including a vibration damper to increase comfort
for crew and passengers. Additionally, the crew is protected by
armor plating. Due to an engine load sharing system, the Mi-17
is capable of single-engine flight in the event of a power failure
by one engine. If one engine should fail, the output of the other
is automatically increased to continue flight. This transport
version of the MI-17 helicopter is intended to carry cargoes in
the cargo compartment or up to 24 fully equipped soldiers.
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Function: |
Transport helicopter |
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Dimensions (rotor diameter/length/height
in flight): |
21.3 m / 18.4 m / 5.7 m |
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Weight: |
11,100 kg takeoff weight (13,000
kg max.) |
|
Engines: |
2 x Isotov TV3-117MT turboshaft
with 1,950 hp each |
|
Cruising speed: |
240 km/h |
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Max. speed: |
250 km/h |
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Vertical climb rate: |
9 m/s |
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Payload: |
24 fully equipperd soldiers
or payload of 4,000 kg |
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Range: |
495 km |
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Ceiling: |
5300 m |
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Armor: |
only crew compartment is protected
against small arms fire |
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Crew: |
3 (2x pilots, 1x flight engineer) |
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Armament: |
None |
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Manufacturer: |
Kazan Helicopter Production
Association; Russia |