Base data
Type: Helicopter (Turbine)
Make: Mil
Model: MI-8 MSB
Year built: 2020
Location: United Kingdom
Price: on request
Engine(s)
Number of engines: 1
Preferential performance of the Mi-8msb helicopter relative to the Mi-17 helicopter

The ability to operate the helicopter at altitudes up to 7300 meters.

Providing basing at altitudes up to 4600 meters with the possibility of complete shutdown of the engines.

Reducing the hourly fuel consumption by 20 %, which allows you to increase the range, or increase the amount of commercial load.

Reduced operating and maintenance costs.

The preparation for the launch of the helicopter (Mi-8MSB √ 5 minutes, the Mi-17 √10 minutes).

At an altitude of 500 meters Lth mi-8MSB helicopter do not differ from similar characteristics of the Mi-17.

LTH:

Modification of the Mi-8MSB

The rotor diameter, m 21.30

The tail rotor diameter, m 3.91

Length, m 18.42

Height, m 5.34

Weight, kg

empty

normal takeoff 11100

maximum takeoff 12500

Engine type 2 GTE Motor-Sich TV3-117VMA-SBM1V 4E ser.

Power, HP 2 x 1500

Maximum speed, km/h 260

Cruising speed, km/h 225

Practical range, km 600

Rate of climb, m/min

Practical ceiling, m 9150

Static ceiling, m 2400

Crew, people 2-3

Payload: up to 24 passengers or 12 stretchers with accompanying or 4000 kg of cargo in the cabin or 3000 kg on the suspension