Abstract

An analysis of circuit design for a perspective propulsion system for short and medium range aircrafts has been carried
 out. It has been shown that use of traditional schemes engines working at aviation kerosene TC-1 will not allow match the
 ICAO ecological requirements for an aircraft of 2025-2035. Transition to hydrogen or liquefied natural gas allows match
 ICAO requirements for CO2 emissions. However it will lead to an essential transportation value addition (due to hydrogen
 and liquefied natural gas production and storage infrastructure). Application of the combined propulsion systems using
 both kerosene and cryogenic fuel will allow increase fuel efficiency and reduce CO2 emission by 16% for hydrogen and by
 2.5–4.5% for methane. In such a case partial transition to hydrogen fuel will allow match ICAO requirements at the current
 freight charge.

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