2840-14-510-5167

Turbo-Jet Engine

2840145105167 145105167 ATAR9B6 COMPLET 2840AA8102429

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

2840-14-510-5167 ENGINE,TURBO-JET 2840145105167 145105167

Managed by France
NSN Created on 4 Nov 1998
Data Last Changed
July 2023
NATO Update Count
1
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2840-14-510-5167 Related Documents Related Documents 2840-14-510-5167 4+ Documents (More...)

ATAR9B6 COMPLET 2840AA8102429 A continuous-combustion type power unit, may be with or without container
RQST NE Updated Every Day 2840-14-510-5167 RQST Updated Every Day 2840-14-510-5167 RQST NE Related Documents
2840-14-510-5167 4+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-510-5167
Day 2840-14-325-6736 RQST NE Related Documents https//www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-510-5167
Turbo-Jet Engine 2840145105167 145105167 | RNVC: 2 | DAC: 2 31 Jan 1990 2840-14-510-5167 https/
2840 Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components from France (FR) 1990 2840-14-510-5167
Engines, Aircraft, Prime Moving; and Components https//www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-510-5167
Turbo-Jet Engine 2840145105167 145105167 Turbines and Jet Engines, Aircraft, Prime Moving; and
11 Aug 1982 2840-14-437-3882 Access Cover 501-219-006-0RNCC: 3 | RNVC: 2 | DAC: 2 31 Jan 1990 2840-14-510-5167

2840-14-510-5167 Demil Restrictions 2840-14-510-5167

DEMIL: | DEMILI: | CRITICALITY: | HMIC: | PMIC: | EDC: | ADPEC:

2840-14-510-5167 is a Turbo-Jet Engine

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