Mi-8T

Helicopter Mi-8T

Mi-8 is a multifunctional helicopter. The helicopter can be used in a variety of conditions and temperatures (from -50 to +50 degrees Celsius), is easy to operate and maintain.

The development of the V-8 (Mi-8) helicopter began at the Pushkin Museum. Mil (now JSC Mil Moscow Helicopter Plant, part of the Russian Helicopters holding) replaced the proven multi-purpose piston Mi-4 helicopter in May 1960. The Mi-8 was developed as a deep upgrade. Mi-4 with a gas turbine engine. The helicopter was developed simultaneously in two modifications: the passenger Mi-8P and the transport Mi-8T.

In the meantime, there is no need to worry about it. ”

FLIGHT CHARACTERISTICS OF MI-8T
Crew 3 people

The maximum speed is 250 km / h.

Cruising speed at normal flight weight is 220 km / h.

Maximum flight altitude with passengers - 3000 m.

Flight range in transport version without additional fuel tanks is 450 km.

The maximum take-off weight is 12,000 kg.

Maximum payload - 4000 kg

The maximum load weight of the external sling is 3000 kg.

Maximum load weight lifted by side boom - 150 kg

Mi-8MTV

FLIGHT CHARACTERISTICS OF MI-8MTV

Crew, people - 3

Passengers, pers. - 22

Flight range, km-1150

Maximum radius of flight range with return to the point of departure (km) - 575

MASSES AND LOADS

Maximum takeoff weight, kg -13000

Empty helicopter weight, kg - 7200

Maximum load in the cargo compartment, kg - 4000

Maximum load on an external sling, kg -4000

Fuel stock in the main tanks -2600 l (2080 kg)

Fuel supply in the main and additional (internal or external) tanks -4400 l (3520 kg)

FLIGHT DATA

Maximum speed, km / h -250

Cruising speed, km / h -230

Dynamic ceiling, m -6000

MI-8PS

The Mi-8 PS helicopter has a comfortable cabin for 14 passengers. Has two doors with folding ladders.

For now, don't worry. "

FLIGHT CHARACTERISTICS OF MI-8PS
For now, don't worry. "
Crew 3 people

The maximum speed is 250 km / h.

Cruising speed at normal flight weight is 220 km / h.

Maximum flight altitude with passengers - 3000 m.

Flight range in transport version without additional fuel tanks is 450 km.

The maximum take-off weight is 12,000 kg.

Maximum payload - 4000 kg

The maximum load on the external sling is 3000 kg.

Maximum load weight lifted by side boom - 150 kg

MI-26

Flight technical characteristics of the Mi-26

Main rotor diameter, m 32.00

Tail rotor diameter, m 7.61

Length, m 40.03

Height, m 8.145

Width, m 3120

Weight, kg

empty 28000

normal takeoff 49600

maximum takeoff 56000

Engine type 2 GTD ZMKB Progress D-136-2

Power, h.p. 2 x 11650

Maximum speed, km / h 290

Cruising speed, km / h 255

Practical range, km 2000

Range of action, km

with filling the main fuel tanks 800

with filling the main and additional. fuel tanks 1905

Practical ceiling, m 4600

Static ceiling, m 1500

Crew, persons 2 + 1

Payload: up to 120 passengers or 20,000 kg of cargo in the cab or suspended

• Modification of the Mi-26T2V

• Main rotor diameter, m 32.00

• Tail rotor diameter, m 7.61

• Length, m 40.03

• Height, m 8.145

• Width, m 3120

• Weight, kg

• empty 28000

• normal takeoff 49600

• maximum takeoff 56000

• Engine type 2 GTD ZMKB Progress D-136-2

• Power, h.p. 2 x 11650

• Maximum speed, km / h 290

• Cruising speed, km / h 255

• Practical range, km 2000

• Range of action, km

• with filling the main fuel tanks 800

• with filling the main and additional. fuel tanks 1905

• Practical ceiling, m 4600

• Static ceiling, m 1500

• Crew, persons 2 + 1

• Payload: up to 120 passengers or 20,000 kg of cargo in the cab or suspended

l-410 NG (Turbolet)

Universal twin-engine aircraft Let L-410 Turbolet

Let L-410 is a nineteen-seat aircraft for local airlines, designed to operate on unprepared unpaved, grassy, ​​snowy areas, as well as on airfields with short runways. Other names: L-410, Let L-410, Turbolet, colloquial names - Cheburashka, Elka, Ellie.

It is planned to launch serial production of the L-410 in Russia on the basis of the Ural Civil Aviation Plant (Yekaterinburg), where a certification check was carried out in order to include the production of the L 410 UVP-E20 aircraft in the list of permitted works to the approval certificate of the production organization.

In the meantime, there is no need to know about it. ”

• L-410NG - development of the L-410UVP-E20 + integral wing tanks + almost 2 times more flight range + more powerful engines + increased volume of the front luggage compartment + the cockpit is equipped with the most modern avionics

L-410UVP-E20 specifications:

• Crew - 2 pilots

  Payload - 19 passengers or 1800 kg cargo

  Engine type - 2 × TVD GE H80-200

  Takeoff power - 2 × 800 HP

  Propeller type - 2 × AVIA AV-725

  The number of blades on each propeller - 5

  Propellers diameter - 2.3 m

  Wingspan - 19.98 m

  Plane length - 14.42 m

  Aircraft height - 5.83 m

  Wing area - 34.86 m2

  Empty aircraft weight - 4050 kg

  Maximum takeoff weight - 6600 kg

  Fuel weight (main tanks) - 1000 kg

  Fuel weight (end tanks) - 313.8 kg

  Maximum speed - 335 km / h IS

  Practical range - 1500 km

  Service ceiling - 4200 m