2840-14-478-1654

Turbo-Jet Engine

2840144781654 144781654 307-175-101-0

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

2840-14-478-1654 ENGINE,TURBO-JET 2840144781654 144781654

Managed by France
NSN Created on 11 Oct 1995
Data Last Changed
July 2023
NATO Update Count
1
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307-175-101-0 A continuous-combustion type power unit, may be with or without container, designed to
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2840-14-478-1654 4+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-478-1654
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Turbo-Jet Engine 2840144781654 144781654 Documents 2840-14-478-1654 2+ Documents ( More... ) https
Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components from France (FR) Nov 1978 2840-14-478-1654
Turbines and Jet Engines, Aircraft, Prime Moving; https//www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-478-1654
Turbo-Jet Engine 2840144781654 144781654 Turbines and Jet Engines, Aircraft, Prime Moving; and
29 Nov 1983 2840-14-352-9263 Turbo-Jet Engine ATAR08C2RNCC: 3 | RNVC: 2 | DAC: 6 14 Nov 1978 2840-14-478-1654

2840-14-478-1654 Demil Restrictions 2840-14-478-1654

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2840-14-478-1654 is a Turbo-Jet Engine

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