2840-14-323-7570

Turbo-Jet Engine

2840143237570 143237570 ATAR09C7 RVS02-02-010-C7

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

2840-14-323-7570 ENGINE,TURBO-JET 2840143237570 143237570

Managed by France
NSN Created on 1 Jan 1975
Data Last Changed
July 2023
NATO Update Count
1
NATO Data Quality
2840-14-323-7570 ENGINE,TURBO-JET 2840143237570 143237570 1/1
NSN 2840-14-323-7570 (Generic Image) 1/1

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2840-14-323-7570 Related Documents Related Documents 2840-14-323-7570 4+ Documents (More...)

ATAR09C7 RVS02-02-010-C7 A continuous-combustion type power unit, may be with or without container,
RQST NE Updated Every Day 2840-14-323-7570 RQST Updated Every Day 2840-14-323-7570 RQST NE Related Documents
2840-14-323-7570 4+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-323-7570
Day 2840-14-333-1246 RQST NE Related Documents https//www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-323-7570
Turbo-Jet Engine 2840143237570 143237570 | RNVC: 2 | DAC: 4 30 Oct 2000 2840-14-323-7570 https/
2840 Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components from France (FR) 2000 2840-14-323-7570
Day 2840-14-522-4175 RQST NE Related Documents https//www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-323-7570
Turbo-Jet Engine 2840143237570 143237570 Day 2840-14-323-7570 RQST NE Related Documents https//
Nov 1981 2840-14-522-4175 Turbo-Jet Engine 307-175-108-0RNCC: 3 | RNVC: 2 | DAC: 4 30 Oct 2000 2840-14-323-7570

2840-14-323-7570 Demil Restrictions 2840-14-323-7570

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2840-14-323-7570 is a Turbo-Jet Engine

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