Методика расчета термогазодинамических характеристик водородосодержащего углеводородного топлива для силовой установки воздушно-космического самолета

Anton Yurevich Vakulin; Taras Vasilevich Grasko

Metodology for calculating the thermogasdynamic characteristics of a hydrogen-containing hydrocarbon fuel for a propulsion system of an aerospace aircraft

Authors

Anton Yurevich Vakulin VUNC VVS "VVA"
Taras Vasilevich Grasko

Keywords:

aviation fuel; cryogenic fuel; hydrogen; kerosene; biofuel system; aerospace aircraft

Abstract

The article is devoted to the development of a method for calculating the thermogasdynamic characteristics of a hydrogen-containing hydrocarbon fuel for a propulsion system of an aerospace aircraft. The dependences of the fuel characteristics on its chemical formula are obtained, which is the basic for shaping the appearance of the automatic control system of a power plant with a biofuel system.