2840-14-510-5196

Turbo-Jet Engine

2840145105196 145105196 ATAR9K50 COMPLET 2840AA8102498

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

2840-14-510-5196 ENGINE,TURBO-JET 2840145105196 145105196

Managed by France
NSN Created on 4 Nov 1998
Data Last Changed
July 2023
NATO Update Count
1
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2840-14-510-5196 Related Documents Related Documents 2840-14-510-5196 4+ Documents (More...)

ATAR9K50 COMPLET 2840AA8102498 A continuous-combustion type power unit, may be with or without container
RQST NE Updated Every Day 2840-14-510-5196 RQST Updated Every Day 2840-14-510-5196 RQST NE Related Documents
2840-14-510-5196 4+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-510-5196
Day 2840-14-241-9175 RQST NE Related Documents https//www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-510-5196
Turbo-Jet Engine 2840145105196 145105196 | RNVC: 2 | DAC: 5 30 Oct 1984 2840-14-510-5196 https/
2840 Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components from France (FR) 1984 2840-14-510-5196
Engines, Aircraft, Prime Moving; and Components https//www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-510-5196
Turbo-Jet Engine 2840145105196 145105196 Turbines and Jet Engines, Aircraft, Prime Moving; and
4 19 Mar 1986 2840-14-395-7076 Gas Turbine 0298015040RNCC: 3 | RNVC: 2 | DAC: 5 30 Oct 1984 2840-14-510-5196

2840-14-510-5196 Demil Restrictions 2840-14-510-5196

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

2840-14-510-5196 is a Turbo-Jet Engine

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