2840-39-000-0747

Turbo-Jet Engine

2840390000747 390000747 NOMIM 4080400377 MOTOR ARTOUSTE

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

Managed by Romania

NSN Created on 25 Feb 2002

Data Last Changed
July 2023

NATO Update Count
1

NATO Data Quality

2840-39-000-0747 ENGINE,TURBO-JET 2840390000747 390000747 1/1 — NSN 2840-39-000-0747 (Generic Image) 1/1

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2840-39-000-0747 Turbo-Jet Engine 2840390000747 390000747

NOMIM 4080400377 MOTOR ARTOUSTE A continuous-combustion type power unit, may be with or without container
RQST NE Updated Every Day 2840-39-000-0747 RQST Updated Every Day 2840-39-000-0747 RQST NE Related Documents
2840-39-000-0747 2+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/ro 2840-39-000-0747

https//www.nsnlookup.com
/fsg-28/fsc-2840

Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components from Romania (RO)

000-0732 Turbo-Jet Engine MOTOR TURBOREACTOR PTR IAR-95RNCC: 5 | RNVC: 2 | DAC: 4 25 Feb 2002 2840-39-000-0747

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2840-39-000-0736 Turbo-Jet Engine 2840390000736 390000736

Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components from Romania (RO) 2002 2840-39-000-0747