2840-39-000-0748

Turbo-Jet Engine

2840390000748 390000748 NOMIM 4080400386 MOTOR M-632-41M (IAR-99)

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

2840-39-000-0748 ENGINE,TURBO-JET 2840390000748 390000748

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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2840-39-000-0748 Related Documents Related Documents 2840-39-000-0748 3+ Documents (More...)

NOMIM 4080400386 MOTOR M-632-41M (IAR-99) A continuous-combustion type power unit, may be with or without
RQST NE Updated Every Day 2840-39-000-0748 RQST Updated Every Day 2840-39-000-0748 RQST NE Related Documents
2840-39-000-0748 2+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/ro 2840-39-000-0748
2002 2840-39-000-0731 Turbo-Jet Engine MOTOR VIPER 632-41RNCC: 5 | RNVC: 2 | DAC: 4 25 Feb 2002 2840-39-000-0748
Turbo-Jet Engine MOTOR M-632-41M (IAR-99)RNCC: 5 | RNVC: 2 | DAC: 4 25 Feb 2002 2840-39-000-0730
Engines, Aircraft, Prime Moving; and Components from Romania (RO) -39-000-0748 Turbo-Jet Engine MOTOR M-632-41M (IAR-99

2840-39-000-0748 Demil Restrictions 2840-39-000-0748

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2840-39-000-0748 is a Turbo-Jet Engine

2840-39-000-0748 End Users End Users 2840-39-000-0748

Romania (WR)

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