2840-40-000-1157

Turbo-Jet Engine

2840400001157 400001157 AI-25TL AI-25-TL

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 Slovakia

NSN Created on 14 Dec 2005

Data Last Changed
January 2023

NATO Update Count
1

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AI-25TL AI-25-TL A continuous-combustion type power unit, may be with or without container, designed
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