Latest offerings of Mi17 Helicopters

Mi-8AMT/Mi-171(new)

[ See specs of the Mi-171E ]

 

MAKS is an international airshow held at Zhukovsky International Airport,

the home of the Gromov Flight Research Institute in Zhukovsky

2023 Aug. 19-24 at Ramenskoye Airfield just south of Moscow

 

   

General characteristics

•  Crew: Three – two pilots and one engineer •  Capacity: 30 troops or 12 stretchers or 4,000 kg (8,820 lb) cargo internally /5,000 kg (11,023 lb) externally slung.
•  Length: 18.465 m (60 ft 7 in) •  Rotor diameter: 21.25 m (69 ft 10½ in)
•  Height: 4.76 m (15 ft 7¼ in) •  Disc area: 356 m² (3,834 ft²)
•  Empty weight: 7,489 kg (16,510 lb) •  Loaded weight: 11,100 kg (24,470 lb)
•  Max. takeoff weight: 13,000 kg (28,660 lb) •  Powerplant: 2 × Klimov TV3-117VM turboshafts, 1,633 kW (2,190 shp) each

Performance

•  Maximum speed: 250 km/h (135 knots, 155 mph) •  Range: 465 km (251 nmi, 289 mi) (standard fuel)
•  Service ceiling: 6,000 m (19,690 ft) •  Rate of climb: 8 m/s[citation needed] (1,575 ft/min)
Price: $US13.9 million dollars usa  

 

Mi-17 RUSSIAN HELICOPTER sold

 

The MI-17 is a multi role helicopter. It can also be very heavily armed with an extensive array or rockets, missiles and guns. It is often used to air assault infantry forces to attack the point of penetration, reinforce units in contact or disrupt counterattacks. Additional missions include; attack, direct air support, electronic warfare, airborne early warning, medevac, search and rescue, and minelaying.

The Mi-17 helicopter, developed at the Mil Design Bureau from the Mi-8 helicopter, is in serial manufactured at the Kazan Helicopter Production Association. The designation Mi-17 is for export; the Russian armed forces called it Mi-8MT. The Mi-17 can be recognized because it has the tail rotor at the starboard side, instead of the port side. The Mi-17 added a number of improvements, including a vibration damper to increase comfort for crew members and passengers. The helicopter has a high thrust-to-weight ratio pair of TVZ-117MT or TVZ-117VM shaft-turbine engines with takeoff power of 1,900 hp. It is capable of single-engine flight in the event of loss of power by one engine (depending on aircraft mission weight) because of an engine load sharing system. If one engine fails, the other engine’s output is automatically increased to allow continued flight which is why these helicopters are in demand and the fact they are outstanding in endurance and reliability.. 

   
   
   

 

 

The Mi-17 is capable of carrying cargoes in the cabin (including long cargo) with half-open or removed doors, external loads, or passengers (24 people). The Mi-17 can carry up to 30 troops and up to 20 wounded; it can also be used for in-flight unloading of special cargoes. The transport version of the MI-17 helicopter is intended to carry cargoes (loads) in the cargo compartment, including long-size cargo with partially- opened or removed cargo doors, external loads, or executives (up to 24 persons). Interior seats are removable for cargo carrying. The rear clamshell doors open, an internal winch facilitates loading of heavy freight. Floor has tie down rings throughout. The aircraft carries a rescue hoist capable to 150 kg.

External stores are mounted on weapons racks on each side of the fuselage. The Mi-17 has six external hardpoints. The helicopter may be provided with longrange communication equipment and a radar, and it can carry equipment with phased-array antennas for suppression of enemy electronic attack and air defence facilities, such as airborne radars, air defence (artillery) weapons control radars, surveillance and target detection radars and missile radar homing heads. The ECM equipment can work both in the reconnaissance and ECM modes or in the reconnaissance mode.

 MI-17 SPECS: Diameter of the bearing screw, m 21,294
Length of the helicopter, m 18,424 Height of the helicopter, m 4,755
Normal take-off weight, kg 11 100 The maximal take-off weight, kg 13 000
The maximal useful loading, kg 4000 Impellent installation (number, type of engines) two ТВЗ-117МТ (2х1900л.с.)
The maximal speed, km/h 250 Static ceiling, m 5000
Practical range, km 495  

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