There is 1 images added on 16 June 2015
Mi-8AMTSh-V  
Initial Operational Capability (IOC): 2015
Maiden Flight: 2014
Total Production: ?
Origin: Russia
Corporations: Mil Helicopter, Russian Helicopters and Ulan-Ude Aviation Plant
Parent System: Mi-8
Initial Operational Capability (IOC): 1967
Maiden Flight: 7 July 1961
Total Production: 12,616
Family Members: Mi-14, Mi-171A1, Mi-171A2, Mi-171M, Mi-171Sh, Mi-17V-5, Mi-8, Mi-8AMTSh-VA and Mi-8MTPR1
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Description: The MIL Mi-8, dubbed Hip by NATO, is a twin-engine, multi-role, medium transport helicopter capable of transporting troops and equipment or conducting ground attack missions. Besides, the aircraft is also suitable for civilian operators related to a variety of transportation roles. The Mi-8 was developed in the late 1950s and 1960s by the Soviet Union, first flew on July 7, 1961, entering service in 1967. The five-bladed main rotor is driven by either two TV2-117 or TV3-117 turboshaft engines rated from 1,700-shp to 2,200-shp allowing a top speed of 230-250 kilometers per hour. In addition to its crew of two/three men, the standard Mi-8 can transport as many as 24/28 troops. The Mi-17 was the export designation for the Soviet Mi-8. The Mi-171 refers to the modern production standard introduced in 1991. The aircraft design and technologies evolved over 60 years with the current production standards (various models) being far more sophisticated and performant than early models. More than 12,000 Mi-8/17/171 helicopters of all models were produced or are in production for the Soviet Union, Russia and international customers. As of November 2013, roughly 2,400 Mi-8/Mi-17 helicopters remain in service worldwide. In January 2015 that figure had increased to 2,469 aircraft with several models remaining in production beyond 2020.

The Russian Air Force Mi-8AMTSh-V is a new version of the Mi-8AMTSh military transport helicopter with upgraded flight capabilities. The aircraft also benefits from the import substitution program which guarantees that all components are Russian made. The new components deliver improved capabilities as well as expanded operational range.

Mi-8AMTSh-V Specifications

Crew: 2
Main Rotor Blades: 5
Number of Engines: 2
Tail Rotor Blades: 3
CEP: Circular Error Probable
Meters (m)   Kilometers (km)   Nautic Miles (nm)   Inch (in)   Yard (yd)   Foot (ft)   Millimeter (mm)
Pound (lb)   Kilogram (kg)   kN (KiloNewton)   Ton (t)
Meters per Second (mps)   Kilometers per Hour (kph)   Knot (kt)   Miles per Hour (mph)
Liter (l)   Galon (gl)
Year (yr)   Minutes (min)   Second (sec)
Shaft-Horse-Power (shp)

Mi-8AMTSh-V News

There is 1 news
on 28 Dec 2015
Monday, December 28, 2015Russian Mi-8AMTSh Assault Helicopters Getting Vitebsk Jammers

Operators & Related Equipment


OperatorsItems

Grand Total ?1
Propulsion Systems
VK-2500x2
Protection Systems
Vitebskx1
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