AIRСРЕДНИЙACTIVE

Mi-17 Hip

RussiaMil Moscow Helicopter PlantВспомогательный вертолётПервый полёт:1994
ОБЗОР СИСТЕМЫ

The Mi-17 Hip-H is a medium twin-turbine utility helicopter produced by Kazan Helicopters, combining the airframe of the Mi-8 with upgraded engines. Powered by two Klimov TV3-117MT turboshafts each producing 1,454 kW, it lifts 4,000 kg internally or 5,000 kg externally. Azerbaijan operates the Mi-17 in the medium utility transport role, supporting troop insertions, logistics resupply, and casualty evacuation. Its excellent performance at altitude and in hot conditions makes it well-suited for operations in the Caucasus mountain environment.

Mi-17 Hip
ПОСМОТРЕТЬ В ПОЛНОМ РАЗМЕРЕ
Mi-17 Hip - Mil
ПРЕИМУЩЕСТВА
  • Most widely operated military helicopter in the world — vast operator experience and parts supply
  • High payload capacity (24 troops or 4,000 kg) for a medium helicopter
  • Dual engine redundancy improves survivability and enables high-altitude operations
  • Can be armed with rockets, gun pods, and ATGMs for light attack missions
  • Proven reliability in extreme climates from Arctic to desert and high-altitude
НЕДОСТАТКИ
  • Limited modern avionics and situational awareness systems in base configuration
  • No inherent self-protection suite — vulnerable without add-on defensive systems
  • High vibration levels compared to modern composite-rotor helicopters
  • High fuel consumption at maximum payload
  • Russian sanctions have complicated spare parts supply for many operators
ТЕХНИЧЕСКИЕ ХАРАКТЕРИСТИКИ
CREW2-3 + 24 Troops Or 4,000 Kg Cargo
RANGE950 Km
LENGTH25.35 M
ENGINES2x Klimov TV3-117MT Turboshaft (1,900 Shp Each)
PAYLOAD4,000 Kg Internal Or 4,000 Kg Slung
MAX SPEED250 Km/H
ROTOR DIAMETER21.29 M
SERVICE CEILING6,000 M
MAX TAKEOFF WEIGHT13,000 Kg
СЕМЕЙСТВО СИСТЕМ2 ВАРИАНТЫ
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