AI-450M/M1/M-В Turboshaft


Designed for use on helicopters of various applications in the load-carrying capacity class of 1,500 … 4,000 kg. Installed on the Mi-2M, МSB-2. In commercial production since 2015.

ACS settings options АI-450М/М1 АI-450М-P/ М1-P АI-450М-B
30-minute maximum power H=0, Vn=0, ISA.
Power, hp 400 465 430
Supports up to temperature, 0С 40 30 40
Taking off power H=0, Vn=0, ISA
Power, hp 400 465 430
Supports up to temperature, 0С 30 15 25
Specific fuel consumption, kg/h/hp 0.280 0.270 0.284
Maximum cruising regime
Power, hp 285 300 300
Supports up to temperature, 0С 30 30 25
Specific fuel consumption, kg/h/hp 0.320 0.312 0.320
Weight, kg 115
Dimensions, mm 1,115 x 648 x
534
1,120 x 684 x
545
Specified service life, h 12,000

Type Certificate of the State Service of Ukraine

The Certificate of the Aviation Register of the Interstate Aviation Committee

The Major Сhange Approval of the Aviation Register of the Interstate Aviation Committee

Applicability

  • Mi-2М

    Mi-2М

  • MSB-2

    MSB-2