2840-39-000-0743

Turbo-Jet Engine

2840390000743 390000743 NOMIM 4080400332 MOTOR SPAY 512-14DW

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

2840-39-000-0743 ENGINE,TURBO-JET 2840390000743 390000743 1/1 — NSN 2840-39-000-0743 (Generic Image) 1/1

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2840-39-000-0743 Turbo-Jet Engine 2840390000743 390000743

NOMIM 4080400332 MOTOR SPAY 512-14DW A continuous-combustion type power unit, may be with or without
RQST NE Updated Every Day 2840-39-000-0743 RQST Updated Every Day 2840-39-000-0743 RQST NE Related Documents
2840-39-000-0743 2+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/ro 2840-39-000-0743

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

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

2002 2840-39-000-0727 Turbo-Jet Engine NOMIM 4080400163RNCC: 2 | RNVC: 2 | DAC: 4 25 Feb 2002 2840-39-000-0743

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

2840-39-000-0733 Turbo-Jet Engine 2840390000733 390000733

Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components from Romania (RO) 2002 2840-39-000-0743