2840-14-549-6962

Turbo-Jet Engine

2840145496962 145496962 307-797-006-0

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

2840-14-549-6962 ENGINE,TURBO-JET 2840145496962 145496962

Managed by France
NSN Created on 27 Apr 2006
Data Last Changed
July 2023
NATO Update Count
1
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2840-14-549-6962 Related Documents Related Documents 2840-14-549-6962 5+ Documents (More...)

Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components from France (FR) Jan 1964 2840-14-549-6962
| RNVC: 2 | DAC: 6 4 Nov 1998 2840-39-000-0738 https//www.nsnlookup.com /fsg-28/fsc-2840/fr 2840-14-549-6962
Turbo-Jet Engine 2840145496962 145496962 www.nsnlookup.com /nato/nato-stock-numbers/inc Turbo-Jet
https//www.nsnlookup.com /nato/nato-stock-numbers/inc Turbo-Jet Engine (INC 02007) Feb 2002 2840-14-549-6962
0738 Turbo-Jet Engine MOTOR TURBOREAT.SPAY 512(ROMBAC)RNCC: 5 | RNVC: 2 | DAC: 4 25 Feb 2002 2840-14-549-6962
31 Jan 1990 2840-14-206-6032 Piston Ring 502-705-300-0RNCC: 3 | RNVC: 2 | DAC: 2 1 Jan 1964 2840-14-549-6962

2840-14-549-6962 Demil Restrictions 2840-14-549-6962

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

2840-14-549-6962 is a Turbo-Jet Engine

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