2840-39-000-0728

Turbo-Jet Engine

2840390000728 390000728 NOMIM 4080400172 MOTOR R11F-300

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

2840-39-000-0728 ENGINE,TURBO-JET 2840390000728 390000728

Managed by Romania
NSN Created on 25 Feb 2002
Data Last Changed
July 2023
NATO Update Count
1
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NOMIM 4080400172 MOTOR R11F-300 A continuous-combustion type power unit, may be with or without container
RQST NE Updated Every Day 2840-39-000-0728 RQST Updated Every Day 2840-39-000-0728 RQST NE Related Documents
2840-39-000-0728 4+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/ro 2840-39-000-0728
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Turbo-Jet Engine 2840390000728 390000728 your web browser . 2840-39-000-0728Turbo-Jet Engine2840390000728
390000728 NOMIM 4080400172 MOTOR R11F /fsg-28/fsc-2840/ro 2840-39-000-0728 Turbo-Jet Engine 2840390000728390000728
Every Day 5935-99-255-1842 RQST NE Restrictions https//www.nsnlookup.com /fsg-28/fsc-2840/ro 2840-39-000-0728
Turbo-Jet Engine 2840390000728 390000728 fsc-5120/fr 5120-14-489-4886 Socket Wrench Socket 5120144894886
Connector5935992551842 992551842 0051112 https//www.nsnlookup.com https//www.nsnlookup.com /fsg-28/fsc-2840/ro 2840-39-000-0728
2002 2840-39-000-0729 Turbo-Jet Engine NOMIM 4080400181RNCC: 2 | RNVC: 2 | DAC: 4 25 Feb 2002 2840-39-000-0728
Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components from Romania (RO) 2002 2840-39-000-0728

2840-39-000-0728 Demil Restrictions 2840-39-000-0728

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2840-39-000-0728 is a Turbo-Jet Engine

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Romania (WR)

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