2840-15-152-0757

Turbo-Jet Engine

2840151520757 151520757 A-1044013-101

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

2840-15-152-0757 ENGINE,TURBO-JET 2840151520757 151520757

Managed by Italy
NSN Created on 3 Aug 2000
Data Last Changed
July 2023
NATO Update Count
1
NATO Data Quality
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A-1044013-101 A continuous-combustion type power unit, may be with or without container, designed to
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2840-15-152-0757 4+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/it 2840-15-152-0757
Day 2840-15-135-5550 RQST NE Related Documents https//www.nsnlookup.com /fsg-28/fsc-2840/it 2840-15-152-0757
Turbo-Jet Engine 2840151520757 151520757 ) https//www.nsnlookup.com /fsg-28/fsc-2840/it https//
Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components from Italy (IT) Jun 2001 2840-15-152-0757
CRITICALITY : | HMIC : | PMIC : | EDC: | ADPEC https//www.nsnlookup.com /fsg-28/fsc-2840/it 2840-15-152-0757
Turbo-Jet Engine 2840151520757 151520757 Components from Italy (IT) Jun 2001 2840-15-152-0757 https
5 9 Oct 1996 2840-15-154-4606 Turbo-Jet Engine 2104F244RNCC: 5 | RNVC: 9 | DAC: 1 6 Jun 2001 2840-15-152-0757

2840-15-152-0757 Demil Restrictions 2840-15-152-0757

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2840-15-152-0757 is a Turbo-Jet Engine

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