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 4+ Documents (More...)

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
6 Feb 1997 2840-14-510-1411 Turbo-Jet Engine ECU102 SECRNCC: 3 | RNVC: 2 | DAC: 6 4 Nov 1998 2840-39-000-0738
www.nsnlookup.com /nato/nato-stock-numbers/inc Turbo-Jet Engine (INC 02007) 0738 Turbo-Jet Engine MOTOR TURBOREAT.SPAY 512(ROMBAC
6 Feb 1997 2840-14-510-1411 Turbo-Jet Engine ECU102 SECRNCC: 3 | RNVC: 2 | DAC: 6 4 Nov 1998 2840-39-000-0738
Turbo-Jet Engine MOTOR TURBOREAT.SPAY 512(ROMBAC)RNCC: 5 | RNVC: 2 | DAC: 4 25 Feb 2002 2840-14

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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