2840-99-147-2639

Turbo-Jet Engine

2840991472639 991472639 RB199MK104 012QD-048 993047082

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 United Kingdom

NSN Created on 2 Mar 1996

Data Last Changed
January 2023

NATO Update Count
1

NATO Data Quality

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