2840-39-000-0730

Turbo-Jet Engine

2840390000730 390000730 NOMIM 4080400199 MOTOR TURBOREACTOR PTR IAR-93P

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

2840-39-000-0730 ENGINE,TURBO-JET 2840390000730 390000730

Managed by Romania
NSN Created on 25 Feb 2002
Data Last Changed
July 2023
NATO Update Count
1
NATO Data Quality
2840-39-000-0730 ENGINE,TURBO-JET 2840390000730 390000730 1/1
NSN 2840-39-000-0730 (Generic Image) 1/1

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2840-39-000-0730 Related Documents Related Documents 2840-39-000-0730 3+ Documents (More...)

.. ) https//www.nsnlookup.com /nato/nato-stock-numbers/inc Turbo-Jet Engine (INC 02007) 2004 2840-39-000-0730
-39-000-0748 Turbo-Jet Engine MOTOR M-632-41M (IAR-99)RNCC: 5 | RNVC: 2 | DAC: 4 25 Feb 2002 2840-39-000-0730
26 Apr 1994 2840-14-544-0351 Turbo-Jet Engine CFM56-2CRNCC: 3 | RNVC: 2 | DAC: 4 23 Dec 2004 2840-39-000-0730

2840-39-000-0730 Demil Restrictions 2840-39-000-0730

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2840-39-000-0730 is a Turbo-Jet Engine

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