2840-16-005-2477

Turbo-Jet Engine

2840160052477 160052477 AI-25TLM

A continuous-combustion type power unit, may be with or without container, designed to exert thrust. It's prime physical characteristics include air compressor(s), combustion chamber(s) and gas turbine. The operating principle is as follows: atmospheric air is inducted into the unit at its front, compressed, heated by combustion of a fuel, expanded through the gas turbine, and ejected at high velocity. It may incorporate features to vary direction of the thrust. View more Turbo-Jet Engine

Managed by Czechia

NSN Created on 8 Dec 2005

Data Last Changed
January 2023

NATO Update Count
1

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2840-16-005-2477 ENGINE,TURBO-JET 2840160052477 160052477 1/1 — NSN 2840-16-005-2477 (Generic Image) 1/1

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