2840-39-000-0738

Turbo-Jet Engine

2840390000738 390000738 NOMIM 4080400279 MOTOR TURBOREAT.SPAY 512(ROMBAC)

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

2840-39-000-0738 ENGINE,TURBO-JET 2840390000738 390000738

Managed by Romania
NSN Created on 25 Feb 2002
Data Last Changed
July 2023
NATO Update Count
1
NATO Data Quality
2840-39-000-0738 ENGINE,TURBO-JET 2840390000738 390000738 1/1
NSN 2840-39-000-0738 (Generic Image) 1/1

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2840-39-000-0738 Related Documents Related Documents 2840-39-000-0738 3+ Documents (More...)

NOMIM 4080400279 MOTOR TURBOREAT.SPAY 512(ROMBAC) A continuous-combustion type power unit, may be with
RQST NE Updated Every Day 2840-39-000-0738 RQST Updated Every Day 2840-39-000-0738 RQST NE Related Documents
2840-39-000-0738 2+ Documents ( More... ) https//www.nsnlookup.com /fsg-28/fsc-2840/ro 2840-39-000-0738
2002 2840-39-000-0730 Turbo-Jet Engine NOMIM 4080400199RNCC: 2 | RNVC: 2 | DAC: 4 25 Feb 2002 2840-39-000-0738
Turbo-Jet Engine MOTOR TURBOREAT.SPAY 512(ROMBAC)RNCC: 5 | RNVC: 2 | DAC: 4 25 Feb 2002 2840-39
Engines, Aircraft, Prime Moving; and Components from Romania (RO) 0738 Turbo-Jet Engine MOTOR TURBOREAT.SPAY 512(ROMBAC

2840-39-000-0738 Demil Restrictions 2840-39-000-0738

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2840-39-000-0738 is a Turbo-Jet Engine

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Romania (WR)

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