Calculation of mass characteristics of a fuselage of the unmanned transport aircraft having vertical take off and landing capacity

Аuthors

Dorogov A. V.

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

Abstract

This paper is dedicate to factors which are necessary for taking into account at calculation of mass characteristics of fuselages for manned and unmanned transport planes civil application. Author developed of formula for calculation of mass characteristics of a fuselage of the unmanned transport aircraft having vertical take off and landing capacity. The formula allowing operatively estimate influence of design parameters on mass characteristics of a fuselage.

Keywords:

unmanned, transport, vertical tack off and landing, fuselage

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