2840-14-323-7565

Turbo-Jet Engine

2840143237565 143237565 ATAR09B5 RVS02-02-009-B5

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

2840-14-323-7565 ENGINE,TURBO-JET 2840143237565 143237565

Managed by France
NSN Created on 1 Jan 1975
Data Last Changed
July 2023
NATO Update Count
1
NATO Data Quality
2840-14-323-7565 ENGINE,TURBO-JET 2840143237565 143237565 1/1
NSN 2840-14-323-7565 (Generic Image) 1/1

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ATAR09B5 RVS02-02-009-B5 A continuous-combustion type power unit, may be with or without container,
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2840-14-323-7565 Demil Restrictions 2840-14-323-7565

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2840-14-323-7565 is a Turbo-Jet Engine

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