2840-39-000-0740

Turbo-Jet Engine

2840390000740 390000740 NOMIM 4080400297 MOTOR VIPER MK 632-41

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

2840-39-000-0740 ENGINE,TURBO-JET 2840390000740 390000740

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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2840-39-000-0740 Related Documents Related Documents 2840-39-000-0740 4+ Documents (More...)

NOMIM 4080400297 MOTOR VIPER MK 632-41 A continuous-combustion type power unit, may be with or without
RQST NE Updated Every Day 2840-39-000-0740 RQST Updated Every Day 2840-39-000-0740 RQST NE Related Documents
2840-39-000-0740 2+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/ro 2840-39-000-0740
Feb 2002 2840-39-000-0750 Turbo-Jet Engine MOTOR VK-1FRNCC: 5 | RNVC: 2 | DAC: 4 25 Feb 2002 2840-39-000-0740
-2840 Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components from Romania (RO) 2840-39-000-0740
Turbo-Jet Engine MOTOR VIPER Turbo-Jet Engine MOTOR VK-1FRNCC: 5 | RNVC: 2 | DAC: 4 25 Feb 2002 2840-39-000-0740

2840-39-000-0740 Demil Restrictions 2840-39-000-0740

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2840-39-000-0740 is a Turbo-Jet Engine

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Romania (WR)

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