2840-12-309-9727

Turbo-Jet Engine

2840123099727 123099727 RB199MK105

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

2840-12-309-9727 ENGINE,TURBO-JET 2840123099727 123099727

Managed by Germany
NSN Created on 24 Mar 1987
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
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