Possible ways of modernization of heavy transport helicopter Mi-26

Аuthors

Tischehko M. N., Artamonov B. L.^*

Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

*e-mail: k102@mai.ru; abl-6124554@yandex.ru

Abstract

The 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

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