2840-39-000-0733

Turbo-Jet Engine

2840390000733 390000733 NOMIM 4080400225 MOTOR VIPER 633-47

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

2840-39-000-0733 ENGINE,TURBO-JET 2840390000733 390000733

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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NSN 2840-39-000-0733 (Generic Image) 1/1

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2840-39-000-0733 Related Documents Related Documents 2840-39-000-0733 4+ Documents (More...)

2177 https//www.nsnlookup.com /nato/nato-stock-numbers/inc Turbo-Jet Engine (INC 02007) 1998 2840-39-000-0733
Turbo-Jet Engine MOTOR VIPER Turbo-Jet Engine MARBORE2F3INSTRNCC: 3 | RNVC: 2 | DAC: 6 4 Nov 1998 2840-39-000-0733
2002 2840-39-000-0743 Turbo-Jet Engine NOMIM 4080400332RNCC: 2 | RNVC: 2 | DAC: 4 25 Feb 2002 2840-39-000-0733
Jan 1975 2840-14-510-4208 Turbo-Jet Engine MARBORE2F3INSTRNCC: 3 | RNVC: 2 | DAC: 6 4 Nov 1998 2840-39-000-0733

2840-39-000-0733 Demil Restrictions 2840-39-000-0733

DEMIL: | DEMILI: | CRITICALITY: | HMIC: | PMIC: | EDC: | ADPEC:

2840-39-000-0733 is a Turbo-Jet Engine

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