<1script type='text/javascript'> (function(){ var widget_id = '5KgGChjEBi';var d=document;var w=window;function l(){ var s = document.createElement('script'); s.type = 'text/javascript'; s.async = true; s.src = '//code.jivosite.com/script/widget/'+widget_id; var ss = document.getElementsByTagName('script')[0]; ss.parentNode.insertBefore(s, ss);}if(d.readyState=='complete'){l();}else{if(w.attachEvent){w.attachEvent('onload',l);}else{w.addEventListener('load',l,false);}}})();

Mil Mi 17 for sale

Mil Mi 17 for sale

The Mi-17 is a further development of the Mi-8 with two CCD TVZ-MT takeoff power kW, and improved flight characteristics. Development of the Mi-17 helicopter was completed in 1980 and 1981. it was first showcased on aerospace exhibition in Paris. The Mi-17 is produced Kazan helicopter plant and aviation plant in Ulan-Ude, which was built more than 2000 Mi-17 helicopters of various modifications:

Mi-17 — base multi-purpose transport helicopter;
Mi-P — passenger helicopter, designed to carry 26 passengers; in the cabin are 13 double passenger seats and the wardrobe, Luggage racks above the seats, there are thermal and sound insulation and heating and ventilation systems, with the left side is the door-ladder, and in the rear part there is a hatch for loading baggage;
Mi-17 «Beauty» — passenger helicopter with beauty superior options 11, 9 and 7 passengers, is preparing to release version 86 (how many?) passengers with increased range to cm;
Mi-17M — rescue helicopter, equipped with a side boom with winch SLH-300 to climb on Board or lowering one or two people or cargo weighing 300kg in the hovering mode of up to a height of 55m and a weight capacity kg equipped with a flashlight, and a universal lifting seat with pulse beacon onboard searchlight bbs-GRIS-575 provides the find objects in the night time and site selection for planting;

Get free more information about these and others Mil Mi 17 for sale:

Your country

Leaving the contact information you agree to the Privacy Policy

  • Mi-17-1V — transport helicopter with GTE TVZ-117VM takeoff power kW, maximum lifting capacity 4000kg in the cockpit and 5000kg on the external load and static ceiling m at normal takeoff weight kg, maximum takeoff weight kg. In troop-transport version in the cargo compartment can accommodate 30 paratroopers jump seat, and sanitary version 12 wounded on stretchers or 20 wounded, including 3 on the stretcher and 17 sitting.
  • In troop transport variant on the sides of the fuselage installed pylons with beamed holders era-57 CRVM for mounting 4 blocks BV 20 DRUG caliber 57mm or containers UPK-23-250 with the cannon GSH-23L gun caliber 23mm or bombs caliber up to 500kg, and incendiary bombs. In the openings of the cargo doors and the blisters cabins can be placed 8 guns at the pivot installations, and firing the front and rear hemispheres is provided by two machine gun in the bow and stern of the mobile units. Protection of crew members and shooters provided bronwyne plates. To protect from missiles «air-to-air and ground-to-air helicopter equipped with active and passive protection systems, as the Mi-8MTV-2. For dropping paratroopers cargo sash dismantled and jumps are made through the cargo door and open the sliding door;
  • Mi-171 version of the Mi — 17 helicopter, developed in 1989; is at the aviation plant in Ulan-Ude;
  • Mi-A — helicopter-flying hospital with complex medical equipment to assist in remote areas, the cab is equipped operating room with heat and sound insulation and the necessary equipment with power supply from the auxiliary power unit.
  • Mi-172 — passenger helicopter with GTE TVZ-117VM takeoff power but providing operation of the helicopter with the high platforms, up to 4000m.
  • Mi-17 «environmental laboratory» is designed for the rapid qualitative and quantitative monitoring of the environment and production structures; equipped with a complex apparatus for multispectral mapping of the area and for sensing of the atmosphere and the earth’s surface at various wavelengths, as well as for radiation control and environmental analysis of the area. The helicopter can be equipped with aerial equipment for routine day aerophotography routes and areas with altitudes from 50 to 6000 meters at flight speeds up to 250km/h
  • Mi-17 firefighter for the elimination of fires in residential or remote and inaccessible areas or in the forest, with overflow device with a volume of 2 m3 and fire the trigger device for Besprechung dropping to 20 firefighters to areas of the forest fire mode hovering helicopter at a height of up to 45m;
  • Mi-PL — helicopter-Director of electronic interference (RAP), with phased antenna arrays (PAA) for radiomodule aircraft radar and radar control arms anti-aircraft missile systems, surveillance radars, detection and targeting air defense systems of the enemy. Digital processing system and the formation of interference provides a classification of the irradiating objects and the selection of the most effective types of interference, control RAP is performed by an operator within the crew;
  • Mi-MD is a deep modernization of the Mi-17-1V, characterized externally improved shape of the forward fuselage and the cargo hatch and improvements in design, among which are increased in width of up to 1.25 m of the sliding door in the cockpit from the left side, allowing quick loading and unloading of 36 Marines, the external suspension system, designed to carry cargo 5000kg, the system buoyancy in case of emergency landing on water, consisting of two ballonets on the main supports of the chassis and two ballonets in the bow, filled for 30s and ensure the maintenance of the helicopter afloat for at least 30s; additional tanks, increasing the flight range of up to 1600 km, additional equipment.
The design of the helicopter is basically the same as the Mi-8, with a number of units and systems of the helicopter Mi-14. Mi-17 looks different from the Mi-8 installing the tail rotor on the left side of the tail beam (instead of right at Mi-8) and shortened engine nacelles, the air inlet being supplied with the ROM.

Main rotor to reduce vibration level is equipped with pendulum damper. Rotor blades made of fiberglass, have the same geometric dimensions as the helicopter Mi-8.

The power plant has a system of automatic maintenance of main rotor rpm and system synchronization engines: in case of failure of one engine is continuing flight with one engine running on emergency mode. The helicopter is equipped with auxiliary power unit GTE AI-9V to power the air motor starters when they start and to power the on-Board network with a constant current, when the engines are not running.

The transmission is new gearbox VR-14, developed for the Mi-14. The three-stage gearbox with two freewheel clutches, is independent of the engine oil system; gearbox has dimensions of 1.2 x 0.88 x 1.76 m and dry weight 842.5 kg, designed for transmission of power but, the rotation speed of the output shafts of the motors 15900 rpm, shaft rotor — 192 rpm

The equipment provides pilotage by day and night and in adverse weather conditions. Mi-171 is installed radio communication «Baklan-20» and «Core 1», radio compasses ark-15M and the ARC-UD, Doppler velocity meter and demolition DISS-32-90, aviagorizonta AGK-77 and AGP-V, radio f-037, navigation system A-723, meterdiameter 8A-813. Military variants of the Mi-17 set-up ejection LTC there and dipole reflectors ASO-2 (under the tail boom) and transmitter interference IR systems.

Technical data Mi-17

Powerplant: 2 x CCD TV3-MT NGO them. Klimov power kW, diameter of rotor: 21.29 m, length: 25.35 m, height: 4.76 m, gross weight: kg, top speed: 250km/h, cruising speed: 240km/h, dynamic ceiling: 5000M, stachecki ceiling out of ground effect: m, range: 465km, payload: 3000-5000kg

Get free more information about these and others Mil Mi 17 for sale:

Your country

Leaving the contact information you agree to the Privacy Policy

Технические характеристики вертолетов: Вертолет Ми-8Т

 

Модификация / Modification   Ми-8Т / Mi-8T
Диаметр главного винта, м / The diameter of the main screwm   21.29
Диаметр хвостового винта, м / The diameterof the tail rotorm   3.91
Длина,м / Length   18.17
Высота ,м / Height   5.65
Масса, кг / Weight
  пустого / empty   6625
  нормальная взлетная / normal takeoff   11100
  максимальная взлетная / maximum takeoff   12000
Тип двигателя / Engine type   2 ГТД Климов ТВ2-117А / 2 GTE Klimov TV2-117A
Мощность, кВт / Power, kW   2 х 1257
Максимальная скорость, км/ч / Maximum speed, km/h   250
Крейсерская скорость, км/ч / Cruising speed, km/h   225
Практическая дальность, км / The practical range, km   480
Практический потолок, м / Service ceiling, m   4500
Статический потолок, м / Static ceiling, m   1900
Экипаж, чел / The crew, pers   2-3
Полезная нагрузка: / Useful load:   32 солдата или 12 носилок с сопровождающими или 4000 кг груза в кабине или 3000 кг на подвеске Боевая нагрузка — 1000 кг на 4 узлах подвески: / 32 soldier or 12 stretchers with attendants or 4000 kg of cargo in the cabin or 3000 kg.
Combat load is 1000 kg 4 hardpoints

Вертолет Ми-8АМТ

Модификация   Ми-8АМТ (Mi-171)
Диаметр несущего винта, м   21.29
Диаметр рулевого винта, м   3.91
Длина, м   18.17
Высота ,м   5.65
Масса, кг
  пустого   6800
  нормальная взлетная   11100
  максимальная взлетная   12000
Тип двигателя   2 ГТД Климов ТВ2-117ВМ (ВК-2500)
Мощность, кВт   2 х 1641 (2014)
Максимальная скорость, км/ч   250
Крейсерская скорость, км/ч   225
Практическая дальность, км
  нормальная   610
  с двумя топливными баками   1065
Практический потолок, м   5000
Статический потолок, м   3900
Экипаж, чел   3
Полезная нагрузка:   до 26 пассажиров или 37 десантников или 12 носилок с сопровождающими или 4000 кг груза в кабине или 4000 кг на подвеске

Вертолет Ми-8МТ

Модификация   Ми-8МТ
Диаметр главного винта, м   21.30
Диаметр хвостового винта, м   3.91
Длина,м   18.42
Высота ,м   5.34
Масса, кг
  пустого   7200
  нормальная взлетная   11100
  максимальная взлетная   13000
Тип двигателя   2 ГТД Климов ТВ3-117МТ
Мощность, кВт   2 х 1454
Максимальная скорость, км/ч   250
Крейсерская скорость, км/ч   230
Практическая дальность, км   500
Скороподъемность, м/мин   540
Практический потолок, м   5000
Статический потолок, м   1760
Экипаж, чел   2-3
Полезная нагрузка:   до 24 пассажиров или 12 носилок с сопровождающими или 4000 кг груза в кабине или 4000 кг на подвеске

Вертолет Ми-8МТВ

Модификация   Ми-8МТВ
Диаметр главного винта, м   21.30
Диаметр хвостового винта, м   3.91
Длина,м   18.42
Высота ,м   5.34
Масса, кг
  пустого   7381
  нормальная взлетная   11100
  максимальная взлетная   13000
Тип двигателя   2 ГТД Климов ТВ3-117ВМ
Мощность, кВт   2 х 1639
Максимальная скорость, км/ч   250
Крейсерская скорость, км/ч   230
Практическая дальность, км   500
Скороподъемность, м/мин   540
Практический потолок, м   6000
Статический потолок, м   3980
Экипаж, чел   2-3
Полезная нагрузка:   до 24 пассажиров или 12 носилок с сопровождающими или 4000 кг груза в кабине или 4000 кг на подвеске

Вертолет Ми-17-1В

Модификация   Ми-17-1В (Mi-17-1v)
Диаметр главного винта, м   21.29
Диаметр хвостового винта, м   3.91
Длина,м   18.424
Высота ,м   4.755
Масса, кг
  пустого   7100
  нормальная взлетная   11100
  максимальная взлетная   13000
Внутренние топливо, кг   1450 + 1420
Тип двигателя   2 ГТД Климов ТВ3-117БМ
Мощность, л.с.
  номинальная   2 х 1900
  максимальная   2 х 2200
Максимальная скорость, км/ч   250
Крейсерская скорость, км/ч   240
Практическая дальность, км   950
Боевой радиус действия, км   555
Практический потолок, м   4000
Статический потолок, м   1760
Экипаж, чел   2-3
Полезная нагрузка:   32 солдата или 12 носилок с сопровождающими или 4000 кг груза в кабине или 4000 кг груза на крюке

 

Получите больше информации о продажи вертолетов Ми 17 в наличии и под заказ:

Отметьте галочкой, если Вы согласны с Политикой конфиденциальности

Summary
Aggregate Rating
4 based on 5 votes
Brand Name
Mil helicopters
Product Name
Mil Mi - 17 helicopters for sale

Pin It on Pinterest