Mi-17, M.L.Mil 'Hip-H'

30k Mi-17, lost WEB site;
I
mproved Mi-8, with more powerful engines for 'hot and high' conditions. The designation Mi-17 is for export; the USSR armed forces called it Mi-8MT. The Mi-17 can be recognized because it has the tail rotor at the starboard side, instead of the port side.
PredecessorsModificationsDevelopments

Mi-8		 ?
More Links...
  • The International Workhorse - the Mi-17
  • Kazan Helicopters Plant is a manufacturer of the Mi-17 and its variants
  • RUSSIA INTENDS TO EXPAND EXPORT OF Mi-17-1V HELICOPTERS
  • MAKS-97 overview
  • Mi-17, Mil 'Hip'
  • Mi-17MD HELICOPTER: VERSATILE CAPABILITIES;
    		• Technical data
    Type Mi-17-1VA
    Function utility
    Year 1980
    Crew ?
    Engines 2*2250(1950?)hp Isotov TV-3-117VM
    Rotor Span 21.2m
    Length 25.3m
    Height 4.70m
    Disc Area 365m2
    Empty Weight 7100kg
    Maximum Weight 13000kg
    Speed 262(250?)km/h
    Ceiling 6000(5000?)m
    Range 465(495?)km
    Load 4000kg
    or 24 seats
    Created January 25, 1996
    Modified April 23, 1998
    by Alexandre Savine;    		 Back to
    Main Gate