2840-14-510-5195

Turbo-Jet Engine

2840145105195 145105195 M53-5 SEC 2840AA8102496

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

2840-14-510-5195 ENGINE,TURBO-JET 2840145105195 145105195

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NSN Created on 4 Nov 1998
Data Last Changed
July 2023
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1
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2840-14-510-5195 Related Documents Related Documents 2840-14-510-5195 4+ Documents (More...)

M53-5 SEC 2840AA8102496 A continuous-combustion type power unit, may be with or without container, designed
RQST NE Updated Every Day 2840-14-510-5195 RQST Updated Every Day 2840-14-510-5195 RQST NE Related Documents
2840-14-510-5195 4+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-510-5195
www.nsnlookup.com /fsg-28/fsc-2840 Gas Turbines and https//www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-510-5195
Turbo-Jet Engine 2840145105195 145105195 Documents 2840-14-510-5195 2+ Documents ( More... ) https
Turbines and Jet Engines, Aircraft, Prime Moving; and Components from France (FR) 16 Oct 1978 2840-14-510-5195
Turbines and Jet Engines, Aircraft, Prime Moving; https//www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-510-5195
Turbo-Jet Engine 2840145105195 145105195 Gas Turbines and Jet Engines, Aircraft, Prime Moving;
Jun 1980 2840-14-352-0311 Turbo-Jet Engine 092-001-499-0RNCC: 3 | RNVC: 2 | DAC: 2 16 Oct 1978 2840-14-510-5195

2840-14-510-5195 Demil Restrictions 2840-14-510-5195

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

2840-14-510-5195 is a Turbo-Jet Engine

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