2840-39-000-0739

Turbo-Jet Engine

2840390000739 390000739 NOMIM 4080400288 MOTOR VIPER MK-623M

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

2840-39-000-0739 ENGINE,TURBO-JET 2840390000739 390000739

Managed by Romania
NSN Created on 25 Feb 2002
Data Last Changed
July 2023
NATO Update Count
1
NATO Data Quality
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2840-39-000-0739 Related Documents Related Documents 2840-39-000-0739 5+ Documents (More...)

NOMIM 4080400288 MOTOR VIPER MK-623M A continuous-combustion type power unit, may be with or without
RQST NE Updated Every Day 2840-39-000-0739 RQST Updated Every Day 2840-39-000-0739 RQST NE Related Documents
2840-39-000-0739 3+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/ro 2840-39-000-0739
8405142724919 142724919,623M 8405-14-272-4919 5+ https//www.nsnlookup.com /fsg-28/fsc-2840/ro 2840-39-000-0739
Turbo-Jet Engine 2840390000739 390000739 browser . 2840-39-000-0739Turbo-Jet Engine2840390000739
390000739 NOMIM 4080400288 MOTOR VIPER MK-623M fsc-2840/ro 2840-39-000-0739 Turbo-Jet Engine 2840390000739390000739
and Components from Romania (RO) Engine NOMIM 4080300116RNCC: 2 | RNVC: 2 | DAC: 4 25 Feb 2002 2840-39-000-0739
Definitive Standard RNCC 2 RNVC 2 DAC 4 MOTOR VIPER https//www.nsnlookup.com /fsg-28/fsc-2840/ro 2840-39-000-0739
Turbo-Jet Engine 2840390000739 390000739 in your web browser . 2840-39-000-0739Turbo-Jet Engine2840390000739
2002 2840-39-000-0721 Turbo-Jet Engine NOMIM 4080300116RNCC: 2 | RNVC: 2 | DAC: 4 25 Feb 2002 2840-39-000-0739
-2840 Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components from Romania (RO) 2840-39-000-0739

2840-39-000-0739 Demil Restrictions 2840-39-000-0739

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2840-39-000-0739 is a Turbo-Jet Engine

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Romania (WR)

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