Possible ways of modernization of heavy transport helicopter Mi-26
Aviation technics and technology
Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia
AbstractThe basic opportunity of creation of the perspective heavy transport helicopter of the one-screw circuit with the steering screw is examined. On an example of the requirements in due time declared in American program JTR to flight-technical characteristics of the perspective device, the technical opportunity of their performance is analyzed by deep updating now most load-lifting domestic helicopter Mi-26.
Keywords:the rotary-wing flying device, the flight-characteristics, useful loading, range of flight, helicopter Mi-26, directions of modernization, aerodynamic quality, propulsive factor