2840-99-690-7230

Turbo-Jet Engine

2840996907230 996907230 RB211-535E4-37/12B

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

2840-99-690-7230 ENGINE,TURBO-JET 2840996907230 996907230

Managed by United Kingdom
NSN Created on 10 Oct 2005
Data Last Changed
January 2023
NATO Update Count
1
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