Mi-26

Technical characteristics Mi-26

  • SIZES
    Rotor diameter (m) 32,0
    Blade quantity (pcs) 8

    BASIC POWER GENERATOR CHARACTERISTICS
    Type, power generator model D-136 2×11400 l.s.
    Power generator quantity (pcs) 2

    HIGH-VOLUME CHARACTERISTICS
    Supreme takeoff mass (t) 56,0
    Empty helicopter weight (t) 28,6
    Weight-lift (t) 20,0

    NAVIGABLE TECHNICAL CHARACTERISTICS
    cruise speed (km/h) 255
    flying range with supreme stress load (km) 800
    in case of supreme charge with 4 additional tanks (km) 1920
    Altitude ceiling under conditions of ISA in case of normal takeoff weight,
    Static (BVZ) (not less) (m) 1520
    Altitude ceiling under conditions of ISA in case of normal takeoff weight,
    dynamic (not less) (m) 4600

    SPACE QUANTITY
    flying crew 5

    CARGO HOLD’S SIZE
    length (m) 12,1
    width (m) 3,25
    altitude (m) 3,17
    volume (cubic meter) 135,89